TY - JOUR
T1 - Improvement of Progressive Damage Model to Predicting Crashworthy Composite Corrugated Plate
AU - Ren, Yiru
AU - Jiang, Hongyong
AU - Ji, Wenyuan
AU - Zhang, Hanyu
AU - Xiang, Jinwu
AU - Yuan, Fuh Gwo
N1 - Publisher Copyright:
© 2017, Springer Science+Business Media Dordrecht.
PY - 2018/2/1
Y1 - 2018/2/1
N2 - To predict the crashworthy composite corrugated plate, different single and stacked shell models are evaluated and compared, and a stacked shell progressive damage model combined with continuum damage mechanics is proposed and investigated. To simulate and predict the failure behavior, both of the intra- and inter- laminar failure behavior are considered. The tiebreak contact method, 1D spot weld element and cohesive element are adopted in stacked shell model, and a surface-based cohesive behavior is used to capture delamination in the proposed model. The impact load and failure behavior of purposed and conventional progressive damage models are demonstrated. Results show that the single shell could simulate the impact load curve without the delamination simulation ability. The general stacked shell model could simulate the interlaminar failure behavior. The improved stacked shell model with continuum damage mechanics and cohesive element not only agree well with the impact load, but also capture the fiber, matrix debonding, and interlaminar failure of composite structure.
AB - To predict the crashworthy composite corrugated plate, different single and stacked shell models are evaluated and compared, and a stacked shell progressive damage model combined with continuum damage mechanics is proposed and investigated. To simulate and predict the failure behavior, both of the intra- and inter- laminar failure behavior are considered. The tiebreak contact method, 1D spot weld element and cohesive element are adopted in stacked shell model, and a surface-based cohesive behavior is used to capture delamination in the proposed model. The impact load and failure behavior of purposed and conventional progressive damage models are demonstrated. Results show that the single shell could simulate the impact load curve without the delamination simulation ability. The general stacked shell model could simulate the interlaminar failure behavior. The improved stacked shell model with continuum damage mechanics and cohesive element not only agree well with the impact load, but also capture the fiber, matrix debonding, and interlaminar failure of composite structure.
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U2 - 10.1007/s10443-017-9610-z
DO - 10.1007/s10443-017-9610-z
M3 - Article
AN - SCOPUS:85019055037
SN - 0929-189X
VL - 25
SP - 45
EP - 66
JO - Applied Composite Materials
JF - Applied Composite Materials
IS - 1
ER -