TY - JOUR
T1 - Damage analysis of pseudo-ductile thin-ply UD hybrid composites - a new analytical method
AU - Jalalvand, Meisam
AU - Czél, Gergely
AU - Wisnom, Michael R.
PY - 2015/2/28
Y1 - 2015/2/28
N2 - A new simple analytical approach for predicting all possible damage modes of Uni-Directional (UD) hybrid composites and their stress-strain response in tensile loading is proposed. To do so, the required stress level for the damage modes (fragmentation, delamination and final failure) are assessed separately. The damage process of the UD hybrid can then be predicted based on the order of the required stress for each damage mode. Using the developed analytical method, a new series of standard-thickness glass/thin-ply carbon hybrid composites was tested and a very good pseudo-ductile tensile response with 1.0% pseudo-ductile strain and no load drop until final failure was achieved. The yield stress value for the best tested layup was more than 1130 MPa. The proposed analytical method is simple, very fast to run and it gives accurate results that can be used for designing thin-ply UD hybrid laminates with the desired tensile response and for conducting further parametric studies.
AB - A new simple analytical approach for predicting all possible damage modes of Uni-Directional (UD) hybrid composites and their stress-strain response in tensile loading is proposed. To do so, the required stress level for the damage modes (fragmentation, delamination and final failure) are assessed separately. The damage process of the UD hybrid can then be predicted based on the order of the required stress for each damage mode. Using the developed analytical method, a new series of standard-thickness glass/thin-ply carbon hybrid composites was tested and a very good pseudo-ductile tensile response with 1.0% pseudo-ductile strain and no load drop until final failure was achieved. The yield stress value for the best tested layup was more than 1130 MPa. The proposed analytical method is simple, very fast to run and it gives accurate results that can be used for designing thin-ply UD hybrid laminates with the desired tensile response and for conducting further parametric studies.
KW - A. hybrid
KW - B. delamination
KW - B. fragmentation
KW - C. analytical modelling
UR - http://www.scopus.com/inward/record.url?scp=84912122143&partnerID=8YFLogxK
UR - http://www.sciencedirect.com/science/journal/1359835X
U2 - 10.1016/j.compositesa.2014.11.006
DO - 10.1016/j.compositesa.2014.11.006
M3 - Article
AN - SCOPUS:84912122143
SN - 1359-835X
VL - 69
SP - 83
EP - 93
JO - Composites Part A: Applied Science and Manufacturing
JF - Composites Part A: Applied Science and Manufacturing
ER -