function hlinks=problsel(handles,problname)

% -------------------------------------------------------------------------
% 1D
% -------------------------------------------------------------------------
if strcmp(problname,'Laminated beam single crack (num)')
    load '..\pict\beam_scrack';
    image(beam_scrack); axis off; axis image;
    set(handles.text1,'String','Modeled crack at the distance of 150 mm from the clamp with width of 0.5 mm and depth of 0.4 mm.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 256 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Crack identification in composite beam using causal B-spline wavelets of fractional order, Modelling in Engineering 15(46), 2013, 57-63.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.kms.polsl.pl/mi/pelne_15/08_15_46.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Laminated beam undamaged (exp)')
    load '..\pict\empty';
    image(empty); axis off; axis image;
    set(handles.text1,'String','Undamaged.');
    set(handles.text2,'String','Beam with dimensions of 250x25 mm and thickness of 5.28 mm.');
    set(handles.text3,'String','24-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]4S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the length of 215 mm with a resolution of 44 points in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., The construction of high-order B-spline wavelets and their decomposition relations for fault detection and localisation in composite beams, Scientific Problems of Machines Operation and Maintenance 46(3), 2011, 43-59.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://t.tribologia.eu/plik/spm/spmom-11-v46n3_p043.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminated beam single crack 1 (exp)')
    load '..\pict\beam_single1';
    image(beam_single1); axis off; axis image;
    set(handles.text1,'String','Crack at the distance of 70 mm from the clamp with width of 1 mm and depth of 1 mm.');
    set(handles.text2,'String','Beam with dimensions of 250x25 mm and thickness of 5.28 mm.');
    set(handles.text3,'String','24-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]4S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the length of 215 mm with a resolution of 44 points in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., The construction of high-order B-spline wavelets and their decomposition relations for fault detection and localisation in composite beams, Scientific Problems of Machines Operation and Maintenance 46(3), 2011, 43-59.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://t.tribologia.eu/plik/spm/spmom-11-v46n3_p043.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminated beam single crack 2 (exp)')
    load '..\pict\beam_single2';
    image(beam_single2); axis off; axis image;
    set(handles.text1,'String','Crack at the distance of 150 mm from the clamp with width of 1 mm and depth of 1 mm.');
    set(handles.text2,'String','Beam with dimensions of 250x25 mm and thickness of 5.28 mm.');
    set(handles.text3,'String','24-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]4S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the length of 215 mm with a resolution of 44 points in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., The construction of high-order B-spline wavelets and their decomposition relations for fault detection and localisation in composite beams, Scientific Problems of Machines Operation and Maintenance 46(3), 2011, 43-59.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://t.tribologia.eu/plik/spm/spmom-11-v46n3_p043.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Laminated beam multiple cracks 1 (exp)')
    load '..\pict\beam_multi1';
    image(beam_multi1); axis off; axis image;
    set(handles.text1,'String','Two cracks at the distances of 50 mm from the edge with width of 1 mm and depth of 2 mm and 119 mm from the edge with width of 1 mm and depth of 1 mm.');
    set(handles.text2,'String','Beam with dimensions of 250x25 mm and thickness of 5.28 mm.');
    set(handles.text3,'String','24-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]4S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the length of 215 mm with a resolution of 39 points in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Identification of multiple cracks in composite beams using discrete wavelet transform, Scientific Problems of Machines Operation and Maintenance 45(2), 2010, 41-52.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://t.tribologia.eu/plik/spm/spmom-10v45n2_p-041.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminated beam multiple cracks 2 (exp)')
    load '..\pict\beam_multi2';
    image(beam_multi2); axis off; axis image;
    set(handles.text1,'String','Two cracks at the distances of 86 mm from the edge with width of 1 mm and depth of 1 mm and 149 mm from the edge with width of 1 mm and depth of 1 mm.');
    set(handles.text2,'String','Beam with dimensions of 250x25 mm and thickness of 5.28 mm.');
    set(handles.text3,'String','24-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]4S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the length of 215 mm with a resolution of 39 points in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Identification of multiple cracks in composite beams using discrete wavelet transform, Scientific Problems of Machines Operation and Maintenance 45(2), 2010, 41-52.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://t.tribologia.eu/plik/spm/spmom-10v45n2_p-041.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminated beam multiple cracks 3 (exp)')
    load '..\pict\beam_multi3';
    image(beam_multi3); axis off; axis image;
    set(handles.text1,'String','Three cracks at the distances of 86 mm from the edge with width of 1 mm and depth of 2.5 mm, 132 mm from the edge with width of 1 mm and depth of 0.5 mm and 220 mm from the edge with width of 1 mm and depth of 1 mm.');
    set(handles.text2,'String','Beam with dimensions of 250x25 mm and thickness of 5.28 mm.');
    set(handles.text3,'String','24-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]4S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the length of 215 mm with a resolution of 39 points in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Identification of multiple cracks in composite beams using discrete wavelet transform, Scientific Problems of Machines Operation and Maintenance 45(2), 2010, 41-52.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://t.tribologia.eu/plik/spm/spmom-10v45n2_p-041.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Beam large delam. 1-2 (num)')
    load '..\pict\beam_l1_2';
    image(beam_l1_2); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 2-3 (num)')
    load '..\pict\beam_l2_3';
    image(beam_l2_3); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 2nd and 3rd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 3-4 (num)')
    load '..\pict\beam_l3_4';
    image(beam_l3_4); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 3rd and 4th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 4-5 (num)')
    load '..\pict\beam_l4_5';
    image(beam_l4_5); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 4th and 5th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 5-6 (num)')
    load '..\pict\beam_l5_6';
    image(beam_l5_6); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 5th and 6th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 6-7 (num)')
    load '..\pict\beam_l6_7';
    image(beam_l6_7); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 6th and 7th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 7-8 (num)')
    load '..\pict\beam_l7_8';
    image(beam_l7_8); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 7th and 8th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 8-9 (num)')
    load '..\pict\beam_l8_9';
    image(beam_l8_9); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 8th and 9th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 9-10 (num)')
    load '..\pict\beam_l9_10';
    image(beam_l9_10); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 9th and 10th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 10-11 (num)')
    load '..\pict\beam_l10_11';
    image(beam_l10_11); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 10th and 11th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large delam. 11-12 (num)')
    load '..\pict\beam_l11_12';
    image(beam_l11_12); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 11th and 12th layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Beam small delam. 1-2 (num)')
    load '..\pict\beam_sl1_2';
    image(beam_sl1_2); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 2-3 (num)')
    load '..\pict\beam_sl2_3';
    image(beam_sl2_3); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 2nd and 3rd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 3-4 (num)')
    load '..\pict\beam_sl3_4';
    image(beam_sl3_4); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 3rd and 4th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 4-5 (num)')
    load '..\pict\beam_sl4_5';
    image(beam_sl4_5); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 4th and 5th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 5-6 (num)')
    load '..\pict\beam_sl5_6';
    image(beam_sl5_6); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 5th and 6th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 6-7 (num)')
    load '..\pict\beam_sl6_7';
    image(beam_sl6_7); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 6th and 7th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 7-8 (num)')
    load '..\pict\beam_sl7_8';
    image(beam_sl7_8); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 7th and 8th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 8-9 (num)')
    load '..\pict\beam_sl8_9';
    image(beam_sl8_9); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 8th and 9th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 9-10 (num)')
    load '..\pict\beam_sl9_10';
    image(beam_sl9_10); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 9th and 10th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 10-11 (num)')
    load '..\pict\beam_sl10_11';
    image(beam_sl10_11); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 10th and 11th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small delam. 11-12 (num)')
    load '..\pict\beam_sl11_12';
    image(beam_sl11_12); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 11th and 12th layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and through-the-width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Beam large lim. delam. 1-2 (num)')
    load '..\pict\beam_il1_2';
    image(beam_il1_2); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 2-3 (num)')
    load '..\pict\beam_il2_3';
    image(beam_il2_3); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 3-4 (num)')
    load '..\pict\beam_il3_4';
    image(beam_il3_4); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 4-5 (num)')
    load '..\pict\beam_il4_5';
    image(beam_il4_5); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 5-6 (num)')
    load '..\pict\beam_il5_6';
    image(beam_il5_6); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 6-7 (num)')
    load '..\pict\beam_il6_7';
    image(beam_il6_7); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 7-8 (num)')
    load '..\pict\beam_il7_8';
    image(beam_il7_8); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 8-9 (num)')
    load '..\pict\beam_il8_9';
    image(beam_il8_9); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 9-10 (num)')
    load '..\pict\beam_il9_10';
    image(beam_il9_10); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 10-11 (num)')
    load '..\pict\beam_il10_11';
    image(beam_il10_11); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam large lim. delam. 11-12 (num)')
    load '..\pict\beam_il11_12';
    image(beam_il11_12); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the large area along the length in the range of 85-137 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Beam small lim. delam. 1-2 (num)')
    load '..\pict\beam_isl1_2';
    image(beam_isl1_2); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 2-3 (num)')
    load '..\pict\beam_isl2_3';
    image(beam_isl2_3); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 3-4 (num)')
    load '..\pict\beam_isl3_4';
    image(beam_isl3_4); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 4-5 (num)')
    load '..\pict\beam_isl4_5';
    image(beam_isl4_5); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 5-6 (num)')
    load '..\pict\beam_isl5_6';
    image(beam_isl5_6); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 6-7 (num)')
    load '..\pict\beam_isl6_7';
    image(beam_isl6_7); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 7-8 (num)')
    load '..\pict\beam_isl7_8';
    image(beam_isl7_8); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 8-9 (num)')
    load '..\pict\beam_isl8_9';
    image(beam_isl8_9); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 9-10 (num)')
    load '..\pict\beam_isl9_10';
    image(beam_isl9_10); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 10-11 (num)')
    load '..\pict\beam_isl10_11';
    image(beam_isl10_11); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Beam small lim. delam. 11-12 (num)')
    load '..\pict\beam_isl11_12';
    image(beam_isl11_12); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between 1st and 2nd layer from the bottom on the small area along the length in the range of 95-105 mm from the clamp and on the limited area along the width of a beam.');
    set(handles.text2,'String','Beam with dimensions of 200x10 mm and thickness of 2.4 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 255 nodes on the surface in the half of width of a beam.');
    set(handles.text7,'String','Katunin A., Przystałka P., Detection and localization of delaminations in composite beams using fractional B-spline wavelets with optimized parameters, Eksploatacja i Niezawodnosc - Maintenance and Reliability 16(3), 2014, 385-393.');
    set(handles.text8,'String','Katunin A., Przystałka P., Structural diagnostics of composite beams using optimally selected fractional B-spline wavelets, Intelligent Systems in Technical and Medical Diagnostics, Korbicz J., Kowal M., Eds., Advances in Intelligent Systems and Computing 230, 2014, 475-486.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.ein.org.pl/sites/default/files/2014-03-07.pdf';
    publhlink2='http://dx.doi.org/10.1007/978-3-642-39881-0_40';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
% 2D
% -------------------------------------------------------------------------
elseif strcmp(problname,'Laminate impact damage: A 20J (exp)')
    load '..\pict\A20';
    image(A20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: A 30J (exp)')
    load '..\pict\A30';
    image(A30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: A 40J (exp)')
    load '..\pict\A40';
    image(A40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: B 20J (exp)')
    load '..\pict\B20';
    image(B20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: B 30J (exp)')
    load '..\pict\B30';
    image(B30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: B 40J (exp)')
    load '..\pict\B40';
    image(B40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: C 20J (exp)')
    load '..\pict\C20';
    image(C20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type C (hemispherical R11 mm) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: C 30J (exp)')
    load '..\pict\C30';
    image(C30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type C (hemispherical R11 mm) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: C 40J (exp)')
    load '..\pict\C40';
    image(C40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type C (hemispherical R11 mm) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: D 20J (exp)')
    load '..\pict\D20';
    image(D20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type D (hemispherical R8 mm) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: D 30J (exp)')
    load '..\pict\D30';
    image(D30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type D (hemispherical R8 mm) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: D 40J (exp)')
    load '..\pict\D40';
    image(D40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type D (hemispherical R8 mm) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: E 10J (exp)')
    load '..\pict\E10';
    image(E10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: E 20J (exp)')
    load '..\pict\E20';
    image(E20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: E 30J (exp)')
    load '..\pict\E30';
    image(E30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: E 40J (exp)')
    load '..\pict\E40';
    image(E40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: H 10J (exp)')
    load '..\pict\H10';
    image(H10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type H (conic) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: H 20J (exp)')
    load '..\pict\H20';
    image(H20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type H (conic) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: H 30J (exp)')
    load '..\pict\H30';
    image(H30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type H (conic) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: H 40J (exp)')
    load '..\pict\H40';
    image(H40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type H (conic) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: I 10J (exp)')
    load '..\pict\I10';
    image(I10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type I (bullet-shaped) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: I 20J (exp)')
    load '..\pict\I20';
    image(I20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type I (bullet-shaped) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: I 30J (exp)')
    load '..\pict\I30';
    image(I30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type I (bullet-shaped) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: I 40J (exp)')
    load '..\pict\I40';
    image(I40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type I (bullet-shaped) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Impact damage assessment in composite structures basing on multiwavelet analysis of modal shapes, Indian Journal of Engineering & Materials Sciences, in press.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 5J (exp)')
    load '..\pict\K5';
    image(K5); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 10J (exp)')
    load '..\pict\K10';
    image(K10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 15J (exp)')
    load '..\pict\K15';
    image(K15); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 15 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 20J (exp)')
    load '..\pict\K20';
    image(K20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 25J (exp)')
    load '..\pict\K25';
    image(K25); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 25 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 30J (exp)')
    load '..\pict\K30';
    image(K30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 35J (exp)')
    load '..\pict\K35';
    image(K35); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 35 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: K 40J (exp)')
    load '..\pict\K40';
    image(K40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type K (vertex-oriented immersed granite stone) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: L 25J (exp)')
    load '..\pict\L25';
    image(L25); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type L (edge-oriented immersed granite stone) with impact energy of 25 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: L 30J (exp)')
    load '..\pict\L30';
    image(L30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type L (edge-oriented immersed granite stone) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: L 35J (exp)')
    load '..\pict\L35';
    image(L35); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type L (edge-oriented immersed granite stone) with impact energy of 35 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: L 40J (exp)')
    load '..\pict\L40';
    image(L40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type L (edge-oriented immersed granite stone) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 5J (exp)')
    load '..\pict\M5';
    image(M5); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 10J (exp)')
    load '..\pict\M10';
    image(M10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 15J (exp)')
    load '..\pict\M15';
    image(M15); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 15 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 20J (exp)')
    load '..\pict\M20';
    image(M20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 25J (exp)')
    load '..\pict\M25';
    image(M25); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 25 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 30J (exp)')
    load '..\pict\M30';
    image(M30); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 30 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 35J (exp)')
    load '..\pict\M35';
    image(M35); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 35 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
elseif strcmp(problname,'Laminate impact damage: M 40J (exp)')
    load '..\pict\M40';
    image(M40); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type M (rough surface-oriented immersed granite stone) with impact energy of 40 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.5 mm.');
    set(handles.text3,'String','Unidirectional glass cloth-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis, Archives of Civil and Mechanical Engineering 15(1), 2015, 251-261.');
    set(handles.text8,'String','Katunin A., Zuba M., Influence of the impactor geometry on the damage character in composite structures, Modelling in Engineering 18(49), 2013, 33-39.');
    set(handles.text9,'String','Katunin A., Sznura M., Experimental test rig for the controlled impact tests of composite plates (in Polish), Aparatura Badawcza i Dydaktyczna 18(4), 2013, 297-302.');
    set(handles.text10,'String','Katunin A., Kostka P., Characterisation of impact damage of composite structures using wavelet-based fusion of ultrasonic and optical images, Advanced Composites Letters 23(5), 2014, in press.');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.01.010';
    publhlink2='http://www.kms.polsl.pl/mi/pelne_18/05_18_49.pdf';
    publhlink3='http://abid.cobrabid.pl/download.php?ma_id=685';
    publhlink4='http://www.acletters.org/abstracts/23_5_4.html';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Through-the-width crack (num)')
    load '..\pict\plate_crack';
    image(plate_crack); axis off; axis image;
    set(handles.text1,'String','Modeled through-the-width crack with a depth of 0.5 mm and width of 1 mm.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.64 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Damage identification in composite plates using two-dimensional B-spline wavelets, Mechanical Systems and Signal Processing 25(8), 2011, 3153-3167.');
    set(handles.text8,'String','Katunin A., Przystałka P., Damage assessment in composite plates using fractional wavelet transform with optimized selection of spatial wavelets, Engineering Applications of Artificial Intelligence 30, 2014, 73-85.');
    set(handles.text9,'String','Katunin A., Przystałka P., Meta-optimization method for wavelet-based damage identification in composite structures, Proc. 2014 Federated Conference on Computer Science and Information Systems, 429–438.');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.ymssp.2011.05.015';
    publhlink2='http://dx.doi.org/10.1016/j.engappai.2014.01.003';
    publhlink3='http://dx.doi.org/10.15439/2014F268';
    publhlink4='';
elseif strcmp(problname,'Spatial damage (num)')
    load '..\pict\sqwindow';
    image(sqwindow); axis off; axis image;
    set(handles.text1,'String','Modeled spatial damage with a depth of 0.5 mm.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.64 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Damage identification in composite plates using two-dimensional B-spline wavelets, Mechanical Systems and Signal Processing 25(8), 2011, 3153-3167.');
    set(handles.text8,'String','Katunin A., Przystałka P., Damage assessment in composite plates using fractional wavelet transform with optimized selection of spatial wavelets, Engineering Applications of Artificial Intelligence 30, 2014, 73-85.');
    set(handles.text9,'String','Katunin A., Przystałka P., Meta-optimization method for wavelet-based damage identification in composite structures, Proc. 2014 Federated Conference on Computer Science and Information Systems, 429–438.');
    set(handles.text10,'String','Katunin A., Spatial damage identification in composite plates using %multiwavelets, Journal of Applied Mathematics and Computational Mechanics 12(3), 2013, 69-78.');
    publhlink1='http://dx.doi.org/10.1016/j.ymssp.2011.05.015';
    publhlink2='http://dx.doi.org/10.1016/j.engappai.2014.01.003';
    publhlink3='http://dx.doi.org/10.15439/2014F268';
    publhlink4='http://amcm.pcz.pl/get.php?article=2013_3/art_08.pdf';
elseif strcmp(problname,'Multiple damages (num)')
    load '..\pict\damag3';
    image(damag3); axis off; axis image;
    set(handles.text1,'String','Modeled short crack and two spatial damages with a depth of 0.5 mm.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.64 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Damage identification in composite plates using two-dimensional B-spline wavelets, Mechanical Systems and Signal Processing 25(8), 2011, 3153-3167.');
    set(handles.text8,'String','Katunin A., Przystałka P., Damage assessment in composite plates using fractional wavelet transform with optimized selection of spatial wavelets, Engineering Applications of Artificial Intelligence 30, 2014, 73-85.');
    set(handles.text9,'String','Katunin A., Przystałka P., Meta-optimization method for wavelet-based damage identification in composite structures, Proc. 2014 Federated Conference on Computer Science and Information Systems, 429–438.');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.ymssp.2011.05.015';
    publhlink2='http://dx.doi.org/10.1016/j.engappai.2014.01.003';
    publhlink3='http://dx.doi.org/10.15439/2014F268';
    publhlink4='';
elseif strcmp(problname,'Through-the-width crack (exp)')
    load '..\pict\plate_crack';
    image(plate_crack); axis off; axis image;
    set(handles.text1,'String','Through-the-width crack with a depth of 0.5 mm and width of 1 mm machined using a milling machine.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.64 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Damage identification in composite plates using two-dimensional B-spline wavelets, Mechanical Systems and Signal Processing 25(8), 2011, 3153-3167.');
    set(handles.text8,'String','Katunin A., Przystałka P., Damage assessment in composite plates using fractional wavelet transform with optimized selection of spatial wavelets, Engineering Applications of Artificial Intelligence 30, 2014, 73-85.');
    set(handles.text9,'String','Katunin A., Przystałka P., Meta-optimization method for wavelet-based damage identification in composite structures, Proc. 2014 Federated Conference on Computer Science and Information Systems, 429–438.');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.ymssp.2011.05.015';
    publhlink2='http://dx.doi.org/10.1016/j.engappai.2014.01.003';
    publhlink3='http://dx.doi.org/10.15439/2014F268';
    publhlink4='';
elseif strcmp(problname,'Spatial damage (exp)')
    load '..\pict\sqwindow';
    image(sqwindow); axis off; axis image;
    set(handles.text1,'String','Spatial damage with a depth of 0.5 mm machined using a milling machine.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.64 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Damage identification in composite plates using two-dimensional B-spline wavelets, Mechanical Systems and Signal Processing 25(8), 2011, 3153-3167.');
    set(handles.text8,'String','Katunin A., Przystałka P., Damage assessment in composite plates using fractional wavelet transform with optimized selection of spatial wavelets, Engineering Applications of Artificial Intelligence 30, 2014, 73-85.');
    set(handles.text9,'String','Katunin A., Przystałka P., Meta-optimization method for wavelet-based damage identification in composite structures, Proc. 2014 Federated Conference on Computer Science and Information Systems, 429–438.');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.ymssp.2011.05.015';
    publhlink2='http://dx.doi.org/10.1016/j.engappai.2014.01.003';
    publhlink3='http://dx.doi.org/10.15439/2014F268';
    publhlink4='';
elseif strcmp(problname,'Multiple damages (exp)')
    load '..\pict\damag3';
    image(damag3); axis off; axis image;
    set(handles.text1,'String','Two spatial damages and a short crack with a depth of 0.5 mm machined using a milling machine.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 2.64 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Damage identification in composite plates using two-dimensional B-spline wavelets, Mechanical Systems and Signal Processing 25(8), 2011, 3153-3167.');
    set(handles.text8,'String','Katunin A., Przystałka P., Damage assessment in composite plates using fractional wavelet transform with optimized selection of spatial wavelets, Engineering Applications of Artificial Intelligence 30, 2014, 73-85.');
    set(handles.text9,'String','Katunin A., Przystałka P., Meta-optimization method for wavelet-based damage identification in composite structures, Proc. 2014 Federated Conference on Computer Science and Information Systems, 429–438.');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.ymssp.2011.05.015';
    publhlink2='http://dx.doi.org/10.1016/j.engappai.2014.01.003';
    publhlink3='http://dx.doi.org/10.15439/2014F268';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Al-GFRP-Al struct. impacts (exp)')
    load '..\pict\al_gfrp';
    image(al_gfrp); axis off; axis image;
    set(handles.text1,'String','Three barely visible impact damages with an impact energy of 3, 6 and 9 J.');
    set(handles.text2,'String','Rectangular plate with dimensions of 200x255 mm.');
    set(handles.text3,'String','Hybrid composite with a core of glass fibre-reinforced epoxy-based laminate and face sheets of aluminium alloy.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 190x250 mm with a resolution of 73x51 points.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'GFRP struct. impacts (exp)')
    load '..\pict\gfrp';
    image(gfrp); axis off; axis image;
    set(handles.text1,'String','Three barely visible impact damages with an impact energy of 3, 6 and 9 J.');
    set(handles.text2,'String','Rectangular plate with dimensions of 205x255 mm.');
    set(handles.text3,'String','Glass fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 205x245 mm with a resolution of 59x71 points.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'CFRP stabilizer delaminations (exp)')
    load '..\pict\stabilizer';
    image(stabilizer); axis off; axis image;
    set(handles.text1,'String','Two delaminated areas.');
    set(handles.text2,'String','Recrangular extraction of a verical stabilizer of military aircraft reinforced with stiffeners and containing rivet holes with dimensions of 270x300 mm.');
    set(handles.text3,'String','Carbon fibre-reinforced epoxy-based laminated composite.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 260x300 mm with a resolution of 73x65 points.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Laminate internal void 1 (num)')
    load '..\pict\void1';
    image(void1); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminate internal void 2 (num)')
    load '..\pict\void2';
    image(void2); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminate internal void 3 (num)')
    load '..\pict\void3';
    image(void3); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminate internal void 4 (num)')
    load '..\pict\void4';
    image(void4); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminate internal void 5 (num)')
    load '..\pict\void5';
    image(void5); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminate internal void 6 (num)')
    load '..\pict\void6';
    image(void6); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Laminate internal void 7 (num)')
    load '..\pict\void7';
    image(void7); axis off; axis image;
    set(handles.text1,'String','Modeled two square voids.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 1.5 mm.');
    set(handles.text3,'String','12-layered glass fibre-reinforced epoxy-based laminated composite with a stacking sequence: [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 64x64 nodes on the surface.');
    set(handles.text7,'String','');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Partial local lack of core (exp)')
    load '..\pict\Sand_partlack';
    image(Sand_partlack); axis off; axis image;
    set(handles.text1,'String','Partial local lack of a core with irregular boundaries located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Local lack of core 1 (exp)')
    load '..\pict\Sand_lack1';
    image(Sand_lack1); axis off; axis image;
    set(handles.text1,'String','Local lack of a core with irregular boundaries located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Local lack of core 2 (exp)')
    load '..\pict\Sand_lack2';
    image(Sand_lack2); axis off; axis image;
    set(handles.text1,'String','Local lack of a core with irregular boundaries located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Crack of core 1 (exp)')
    load '..\pict\Sand_crack1';
    image(Sand_crack1); axis off; axis image;
    set(handles.text1,'String','Crack of a core located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Crack of core 2 (exp)')
    load '..\pict\Sand_crack2';
    image(Sand_crack2); axis off; axis image;
    set(handles.text1,'String','Cross-shaped crack of a core located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Through-the-width crack of core (exp)')
    load '..\pict\Sand_tcrack';
    image(Sand_tcrack); axis off; axis image;
    set(handles.text1,'String','Through-the-width crack of a core located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Debonding core-face sheet (exp)')
    load '..\pict\Sand_debond';
    image(Sand_debond); axis off; axis image;
    set(handles.text1,'String','Square-shaped debonding between the core and upper face sheet located at the geometric centre of a plate.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: A 10J (exp)')
    load '..\pict\Sand_A10';
    image(Sand_A10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: A 15J (exp)')
    load '..\pict\Sand_A15';
    image(Sand_A15); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 15 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: A 20J (exp)')
    load '..\pict\Sand_A20';
    image(Sand_A20); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 20 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: A 25J (exp)')
    load '..\pict\Sand_A25';
    image(Sand_A25); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type A (hemispherical R17 mm) with impact energy of 25 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: B 5J (exp)')
    load '..\pict\Sand_B5';
    image(Sand_B5); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: B 7.5J (exp)')
    load '..\pict\Sand_B75';
    image(Sand_B75); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 7.5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: B 10J (exp)')
    load '..\pict\Sand_B10';
    image(Sand_B10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: B 15J (exp)')
    load '..\pict\Sand_B15';
    image(Sand_B15); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type B (hemispherical R14 mm) with impact energy of 15 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: C 7.5J (exp)')
    load '..\pict\Sand_C75';
    image(Sand_C75); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type C (hemispherical R11 mm) with impact energy of 7.5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: C 10J (exp)')
    load '..\pict\Sand_C10';
    image(Sand_C10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type C (hemispherical R11 mm) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: D 5J (exp)')
    load '..\pict\Sand_D5';
    image(Sand_D5); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type D (hemispherical R8 mm) with impact energy of 5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: D 7.5J (exp)')
    load '..\pict\Sand_D75';
    image(Sand_D75); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type D (hemispherical R8 mm) with impact energy of 7.5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: D 10J (exp)')
    load '..\pict\Sand_D10';
    image(Sand_D10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type D (hemispherical R8 mm) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: E 5J (exp)')
    load '..\pict\Sand_E5';
    image(Sand_E5); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: E 7.5J (exp)')
    load '..\pict\Sand_E75';
    image(Sand_E75); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 7.5 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Sandwich impact damage: E 10J (exp)')
    load '..\pict\Sand_E10';
    image(Sand_E10); axis off; axis image;
    set(handles.text1,'String','Impact damage caused by the impactor of type E (hemispherical R5 mm) with impact energy of 10 J in the geometric centre.');
    set(handles.text2,'String','Square plate with dimensions of 300x300 mm and thickness of 4.1 mm.');
    set(handles.text3,'String','Sandwich with a 3 mm core made of aramid paper saturated by phenolic resin with hexagonal cells and face sheets made of glass fibre-reinforced epoxy laminate.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of 250x250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis, Composite Structures 118, 2014, 385-391.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.compstruct.2014.08.010';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Rotor blade: longitudinal crack (num)')
    load '..\pict\rotorbladeh';
    image(rotorbladeh); axis off; axis image;
    set(handles.text1,'String','Modeled through-the-length notch located on the vertical distance of 80 mm with a depth of 0.2 mm.');
    set(handles.text2,'String','A rotor blade with the length of 300 mm and width of 150 mm (in orthogonal plane projection) and a thickness of 2.4 mm.');
    set(handles.text3,'String','Carbon fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 150x200 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Holewik F., Crack identification in composite elements with non-linear geometry using spatial wavelet transform, Archives of Civil and Mechanical Engineering 13(3), 2013, 287-296.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2013.02.003';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Rotor blade: transversal crack (num)')
    load '..\pict\rotorbladev';
    image(rotorbladev); axis off; axis image;
    set(handles.text1,'String','Modeled through-the-width notch located on the horizontal distance of 60 mm with a depth of 0.2 mm.');
    set(handles.text2,'String','A rotor blade with the length of 300 mm and width of 150 mm (in orthogonal plane projection) and a thickness of 2.4 mm.');
    set(handles.text3,'String','Carbon fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 150x200 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Holewik F., Crack identification in composite elements with non-linear geometry using spatial wavelet transform, Archives of Civil and Mechanical Engineering 13(3), 2013, 287-296.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2013.02.003';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Circular plate: surface damage 1 (num)')
    load '..\pict\circplate1';
    image(circplate1); axis off; axis image;
    set(handles.text1,'String','Modeled surface damage with a depth of 0.2 mm.');
    set(handles.text2,'String','Circular plate with radius of 250 mm and a thickness of 2.4 mm.');
    set(handles.text3,'String','Glass fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 50x100 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Vibration-based damage identification in composite circular plates using polar discrete wavelet transform, Journal of Vibroengineering 15(1), 2013, 355-363.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://jve.lt/Vibro/JVE-2013-15-1/JVE-2013-15-1-953.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Circular plate: surface damage 2 (num)')
    load '..\pict\circplate2';
    image(circplate2); axis off; axis image;
    set(handles.text1,'String','Modeled surface damage with a depth of 0.2 mm.');
    set(handles.text2,'String','Circular plate with radius of 250 mm and a thickness of 2.4 mm.');
    set(handles.text3,'String','Glass fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 50x100 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Vibration-based damage identification in composite circular plates using polar discrete wavelet transform, Journal of Vibroengineering 15(1), 2013, 355-363.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://jve.lt/Vibro/JVE-2013-15-1/JVE-2013-15-1-953.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Circular plate: delamination (num)')
    load '..\pict\circplate3';
    image(circplate3); axis off; axis image;
    set(handles.text1,'String','Modeled delamination between first and second layers from the top.');
    set(handles.text2,'String','Circular plate with radius of 250 mm and a thickness of 2.4 mm.');
    set(handles.text3,'String','Glass fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 50x100 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Vibration-based damage identification in composite circular plates using polar discrete wavelet transform, Journal of Vibroengineering 15(1), 2013, 355-363.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://jve.lt/Vibro/JVE-2013-15-1/JVE-2013-15-1-953.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'Circular plate: internal void (num)')
    load '..\pict\circplate4';
    image(circplate4); axis off; axis image;
    set(handles.text1,'String','Modeled internal void in the second layer from the top.');
    set(handles.text2,'String','Circular plate with radius of 250 mm and a thickness of 2.4 mm.');
    set(handles.text3,'String','Glass fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Finite element analysis of modal frequencies with a resolution of displacements of 50x100 nodes on the surface.');
    set(handles.text7,'String','Katunin A., Vibration-based damage identification in composite circular plates using polar discrete wavelet transform, Journal of Vibroengineering 15(1), 2013, 355-363.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://jve.lt/Vibro/JVE-2013-15-1/JVE-2013-15-1-953.pdf';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
elseif strcmp(problname,'Circular plate: stiff inclusion (exp)')
    load '..\pict\stiffincl';
    image(stiffincl); axis off; axis image;
    set(handles.text1,'String','Thin sector-shaped inclusion made of PTFE tape with angular dimension of 20 deg.');
    set(handles.text2,'String','Circular plate with radius of 250 mm and a thickness of 2.1 mm.');
    set(handles.text3,'String','Glass fibre-reinforced epoxy-based laminated composite with a stacking sequence of [0/60/-60]2S.');
    set(handles.text4,'String','Scanned by the laser Doppler vibrometer on the area of R=78-250 mm with a resolution of 64x64 points.');
    set(handles.text7,'String','Katunin A., Identification of stiff inclusion in circular composite plate based on quaternion wavelet analysis of modal shapes, Journal of Vibroengineering 16(5), 2014, 2545-2551.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://www.jve.lt/Vibro/JVE-2014-16-5/JVE01614081352.html';
    publhlink2='';
    publhlink3='';
    publhlink4='';
% -------------------------------------------------------------------------
% 3D
% -------------------------------------------------------------------------
elseif strcmp(problname,'CF-epoxy plate with hole (exp)')
    load '..\pict\ct_cf_epoxy';
    image(ct_cf_epoxy); axis off; axis image;
    set(handles.text1,'String','Delaminations caused by water-jet cutting of a circular hole.');
    set(handles.text2,'String','Rectangluar plate with dimensions of 300x150x5 mm with a circular hole with diameter of 30 mm.');
    set(handles.text3,'String','Carbon fibre-reinforced epoxy-based laminated composite with a stacking sequence of [45/-45]S.');
    set(handles.text4,'String','Scanned by the computed tomograph with a resulted resolution of the region of interest of 452x504x83 voxels.');
    set(handles.text7,'String','Katunin A., Dańczak M., Kostka P., Automated identification and classification of internal defects in composite structures using computed tomography and 3D wavelet analysis, Archives of Civil and Mechanical Engineering, in press, doi: 10.1016/j.acme.2014.08.002.');
    set(handles.text8,'String','');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.08.002';
    publhlink2='';
    publhlink3='';
    publhlink4='';
elseif strcmp(problname,'MLG-epoxy plate with hole (exp)')
    load '..\pict\ct_mlg_epoxy';
    image(ct_mlg_epoxy); axis off; axis image;
    set(handles.text1,'String','Delaminations caused by water-jet cutting of a circular hole.');
    set(handles.text2,'String','Rectangluar plate with dimensions of 800x150x2 mm with a circular hole with diameter of 30 mm.');
    set(handles.text3,'String','Multilayer weft knitted fabrics epoxy-based composite with a stacking sequence of [0/90]S.');
    set(handles.text4,'String','Scanned by the computed tomograph with a resulted resolution of the region of interest of 434x507x100 voxels.');
    set(handles.text7,'String','Katunin A., Dańczak M., Kostka P., Automated identification and classification of internal defects in composite structures using computed tomography and 3D wavelet analysis, Archives of Civil and Mechanical Engineering, in press, doi: 10.1016/j.acme.2014.08.002.');
    set(handles.text8,'String','Grübner B., Hufenbach W., Gottwald R., Lepper M., Zhou B, Experimental and numerical validation of an analytical calculation method for notched fibre-reinforced multilayered composites under bending and compressive loads, Proc. of ICCM19, Montreal 2013, 4543-4552.');
    set(handles.text9,'String','');
    set(handles.text10,'String','');
    publhlink1='http://dx.doi.org/10.1016/j.acme.2014.08.002';
    publhlink2='http://confsys.encs.concordia.ca/ICCM19/list_of_all_accepted_papers.html';
    publhlink3='';
    publhlink4='';
end
hlinks={publhlink1,publhlink2,publhlink3,publhlink4};