TY - JOUR
T1 - Failure modes and strength prediction of thin ply CFRP angle-ply laminates
AU - Yuan, Yanan
AU - Yao, Xuefeng
AU - Liu, Bin
AU - Yang, Heng
AU - Imtiaz, Haroon
N1 - Publisher Copyright:
© 2017 Elsevier Ltd
PY - 2017/9/15
Y1 - 2017/9/15
N2 - In this paper, the tensile strength and failure modes of thin ply carbon fiber-reinforced polymer (CFRP) angle-ply laminates are investigated by experiments and predicted by Finite element method (FEM) and theoretical model. First, experiments are performed to evaluate the tensile behavior of thin ply CFRP angle-ply laminates fabricated with different fiber areal weights of prepreg (20,60,120 g/m2) and ply angle (15°, 30°). Experimental results show that thin ply angle-ply laminates present different failure modes, and also the tensile strengths do not increase monotonically with the decrease in fiber areal weight. Second, both theoretical and FEM models are established to predict the strength and failure modes of thin ply CFRP angle-ply laminates with different ply thickness and fiber volume fraction, also two competing mechanisms finally cause the non-monotonic change of strengths of thin-ply laminates which has good agreement with experimental results. Finally, a failure diagram of thin ply angle-ply laminates under tensile load is given, which shows different failure modes (fiber breakage, delamination and transverse matrix failure) for fiber areal weight (0–240 g/m2) and ply angle (0–90°). Also the delamination is suppressed and the fiber breakage is extended with the decrease of fiber areal weight in the ply angle range of 10°–25°.
AB - In this paper, the tensile strength and failure modes of thin ply carbon fiber-reinforced polymer (CFRP) angle-ply laminates are investigated by experiments and predicted by Finite element method (FEM) and theoretical model. First, experiments are performed to evaluate the tensile behavior of thin ply CFRP angle-ply laminates fabricated with different fiber areal weights of prepreg (20,60,120 g/m2) and ply angle (15°, 30°). Experimental results show that thin ply angle-ply laminates present different failure modes, and also the tensile strengths do not increase monotonically with the decrease in fiber areal weight. Second, both theoretical and FEM models are established to predict the strength and failure modes of thin ply CFRP angle-ply laminates with different ply thickness and fiber volume fraction, also two competing mechanisms finally cause the non-monotonic change of strengths of thin-ply laminates which has good agreement with experimental results. Finally, a failure diagram of thin ply angle-ply laminates under tensile load is given, which shows different failure modes (fiber breakage, delamination and transverse matrix failure) for fiber areal weight (0–240 g/m2) and ply angle (0–90°). Also the delamination is suppressed and the fiber breakage is extended with the decrease of fiber areal weight in the ply angle range of 10°–25°.
KW - Delamination
KW - Failure criterion
KW - Laminate theory
KW - Strength
KW - Thin ply CFRP angle-ply laminates
UR - https://www.scopus.com/pages/publications/85020699139
U2 - 10.1016/j.compstruct.2017.06.005
DO - 10.1016/j.compstruct.2017.06.005
M3 - Article
AN - SCOPUS:85020699139
SN - 0263-8223
VL - 176
SP - 729
EP - 735
JO - Composite Structures
JF - Composite Structures
ER -