TY - JOUR
T1 - Numerical simulation of interlaminar damage propagation in CFRP cross-ply laminates under transverse loading
AU - Nishikawa, Masaaki
AU - Okabe, Tomonaga
AU - Takeda, Nobuo
N1 - Funding Information:
We would like to thank Dr. J. Takatsubo and Dr. N. Toyama (AIST) for their cooperation and valuable comments in the experiment. T.O. acknowledges the support of the Ministry of Education, Culture, Sports, Science and Technology of Japan under Grants-in-Aid for Scientific Research (No. 18760515). M.N. also acknowledges the support of the Ministry of Education, Culture, Sports, Science and Technology of Japan under Grants-in-Aid for Scientific Research (No. 17-11722).
PY - 2007/5/15
Y1 - 2007/5/15
N2 - This paper proposes a numerical simulation of interlaminar damage propagation in FRP laminates under transverse loading, using the finite element method. First, we conducted drop-weight impact tests on CFRP cross-ply laminates. A ply crack was generated at the center of the lowermost ply, and then a butterfly-shaped interlaminar delamination was propagated at the 90/0 ply interface. Based on these experimental observations, we present a numerical simulation of interlaminar damage propagation, using a cohesive zone model to address the energy-based criterion for damage propagation. This simulation can address the interlaminar delamination with high accuracy by locating a fine mesh near the damage process zone, while maintaining computational efficiency with the use of automatic mesh generation. The simulated results of interlaminar delamination agreed well with the experiment results. Moreover, we demonstrated that the proposed method reduces the computational cost of the simulation.
AB - This paper proposes a numerical simulation of interlaminar damage propagation in FRP laminates under transverse loading, using the finite element method. First, we conducted drop-weight impact tests on CFRP cross-ply laminates. A ply crack was generated at the center of the lowermost ply, and then a butterfly-shaped interlaminar delamination was propagated at the 90/0 ply interface. Based on these experimental observations, we present a numerical simulation of interlaminar damage propagation, using a cohesive zone model to address the energy-based criterion for damage propagation. This simulation can address the interlaminar delamination with high accuracy by locating a fine mesh near the damage process zone, while maintaining computational efficiency with the use of automatic mesh generation. The simulated results of interlaminar delamination agreed well with the experiment results. Moreover, we demonstrated that the proposed method reduces the computational cost of the simulation.
KW - Composite material
KW - Cross-ply laminate
KW - Delamination
KW - Finite element method
KW - Transverse loading
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U2 - 10.1016/j.ijsolstr.2006.09.007
DO - 10.1016/j.ijsolstr.2006.09.007
M3 - Article
AN - SCOPUS:33947242756
SN - 0020-7683
VL - 44
SP - 3101
EP - 3113
JO - International Journal of Solids and Structures
JF - International Journal of Solids and Structures
IS - 10
ER -