1. 沈阳航空航天大学民用航空学院,沈阳,110000
2. 沈阳航空航天大学辽宁省高性能聚合物基复合材料重点实验室,沈阳,110000
纸质出版:2023
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崔旭,王祖昊. CFRP 层合板力学性能数值模拟的研究进展[J]. 航空制造技术, 2023, 66(15): 60-70.
CUI Xu, WANG Zuhao. Research Progress on Numerical Simulation of Mechanical Properties of CFRP Laminates[J]. Aeronautical Manufacturing Technology, 2023, 66(15): 60-70.
崔旭,王祖昊. CFRP 层合板力学性能数值模拟的研究进展[J]. 航空制造技术, 2023, 66(15): 60-70. DOI: 10.16080/j.issn1671-833x.2023.15.060.
CUI Xu, WANG Zuhao. Research Progress on Numerical Simulation of Mechanical Properties of CFRP Laminates[J]. Aeronautical Manufacturing Technology, 2023, 66(15): 60-70. DOI: 10.16080/j.issn1671-833x.2023.15.060.
碳纤维增强聚合物基复合材料(Carbon fiber reinforced polymer,CFRP)具有高比模量、高比强度及耐疲劳等优异的性能,被广泛应用于各个领域。但由于其具体的使用环境较为复杂,在服役的过程中易造成损伤而形成安全隐患,为此国内外学者针对CFRP 层合板的力学性能进行了研究。本文从冲击损伤、分层损伤、高低温及湿热老化和多场耦合损伤4 个角度对CFRP 层合板力学性能模拟研究进展进行系统综述,并详细阐述了基于虚拟裂纹闭合技术(VCCT)、内聚力模型(CZM)和渐进损伤本构模型(PDM)等先进数值分析方法模拟CFRP 层合板损伤机理的研究现状。通过对比不同的有限元模拟方法,指出其优势及存在的问题,并对CFRP 层合板力学性能模拟未来的研究方向进行了展望。
Carbon fiber reinforced polymer matrix composites (CFRP) are widely used in various fields because of their excellent properties such as high specific modulus
high specific strength and fatigue resistance. However
due Carbon fiber reinforced polymer matrix composites (CFRP) are widely used in various fields because of their excellent properties such as high specific modulus
high specific strength and fatigue resistance. However
due to its complex use environment
it is easy to cause damage in the process of service and form a safety hazard. For this reason
scholars at home and abroad have studied the mechanical properties of CFRP laminates. The research progress of mechanical properties simulation of CFRP laminates is systematically reviewed from the four perspectives of impact damage
delamination damage
high and low temperature and damp-heat aging and multi-field coupled damage. The research status of CFRP laminate damage mechanism simulation based on advanced numerical analysis methods such as virtual crack closure technology (VCCT)
cohesion zone model (CZM) and progressive damage constitutive model (PDM) is described in detail. By comparing different finite element simulation methods
the advantages and existing problems are pointed out
and the future research direction of the mechanical properties simulation of CFRP laminates is prospected. to its complex use environment
it is easy to cause damage in the process of service and form a safety hazard. For this reason
scholars at home and abroad have studied the mechanical properties of CFRP laminates. The research progress of mechanical properties simulation of CFRP laminates is systematically reviewed from the four perspectives of impact damage
delamination damage
high and low temperature and damp-heat aging and multi-field coupled damage. The research status of CFRP laminate damage mechanism simulation based on advanced numerical analysis methods such as virtual crack closure technology (VCCT)
cohesion zone model (CZM) and progressive damage constitutive model (PDM) is described in detail. By comparing different finite element simulation methods
the advantages and existing problems are pointed out
and the future research direction of the mechanical properties simulation of CFRP laminates is prospected.
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