High Strain Rate Modeling of CFRP Composite Under Compressive Loading

被引:0
|
作者
Chaurasia, Bipin Kumar [1 ]
Kumar, Deepak [1 ]
机构
[1] Natl Inst Technol, Dept Mech Engn, Jamshedpur 831014, India
关键词
CFRP; High strain rate; Hashin failure; VUMAT; NUMERICAL CALIBRATION; ELASTIC STRAINS; SHPB TEST; BEHAVIOR;
D O I
10.14429/dsj.74.19902
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
An in-depth understanding of how Carbon Fiber-Reinforced Plastics (CFRP) respond to intense strain rates is essential, particularly in non-linear deformation and dynamic loading situations. The authors performed a computational study to examine the behavior of CFRP composites when exposed to high strain rates under compressive loading. Specifically, we employed Split Hopkinson Pressure Bar models for cohesive interfacial simulations, continuum shell analysis, and laminated composites oriented at 0 degrees at a strain rate equivalent to 900 s(-1). The Finite Element model utilized a custom Hashin damage model and a Vectorized User Material (VUMAT) sub-routine to identify degradation damage within the CFRP composite model. The quasi-isotropic composite demonstrated a significant enhancement in dynamic strength compared to static values, attributed to its intense sensitivity to strain. As confirmed by experimental test results, numerical simulations accurately predicted stress (sigma)-strain (epsilon) and strain rate ((epsilon) over dot) curves. Additionally, it was observed that the relationship between damage behavior varied depending on the element type used.
引用
收藏
页码:305 / 315
页数:11
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