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A progressive damage fatigue model for unidirectional laminated composites based on Finite Element Analysis: Theory and Practice

机译：基于有限元分析的单向层合复合材料渐进损伤疲劳模型：理论与实践

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Hack M; Carrella-Payan D; Magneville B; Naito T; Urushiyama U; Yokozeki T; Yamazaki W; Van Paepegem Wim;
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年度 2017
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正文语种 eng
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1. A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis [J] . Michael Hack, D. Carrella-Payan, B. Magneville, Frattura e Integrita Strutturale . 2018,第46期

机译：基于有限元分析的单向层合复合材料渐进损伤疲劳模型
2. Implementation of fatigue model for unidirectional laminate based on finite element analysis: theory and practice [J] . D. Carrella-Payan, B. Magneville, M. Hack, Frattura e Integrita Strutturale . 2016,第38期

机译：基于有限元分析的单向层板疲劳模型的实现：理论与实践
3. Progressive Fatigue Damage Simulation in Laminated Composites Based on Explicit Finite Element Formulation [J] . Nikishkov Yuri, Seon Guillaume, Makeev Andrew Journal of the American Helicopter Society . 2019,第2期

机译：基于显式有限元公式的层合复合材料渐进疲劳损伤模拟
4. Multiscale Model for Progressive Damage and Failure of Laminated Composites Using an Explicit Finite Element Method [C] . E. Pineda, A. Waas, B. Bednarcyk, AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference . 2009

机译：层状复合材料渐进破坏和破坏的多尺度模型的显式有限元方法
5. An automated dynamic fracture procedure and a continuum damage mechanics based model for finite element simulations of delamination failure in laminated composites. [D] . Aminjikarai Vedagiri, Srinivasa Babu. 2009

机译：一种自动动态断裂程序和基于连续损伤力学的模型，用于层压复合材料中分层破坏的有限元模拟。
6. A Continuum Damage Model for Intralaminar Progressive Failure Analysis of CFRP Laminates Based on the Modified Puck’s Theory [O] . Jiefei Gu, Ke Li, Lei Su 2019

机译：基于修正圆盘理论的CFRP层压板腹腔内渐进破坏分析的连续损伤模型
7. Implementation of fatigue model for unidirectional laminate based on finite element analysis : theory and practice [O] . Carrella-Payan D., Magneville B., Hack M., 2016

机译：基于有限元分析的单向层合板疲劳模型的实现：理论与实践
8. Progressive Damage Analysis of Laminated Composite (PDALC) (A Computational Model Implemented in the NASA COMET Finite Element Code) [R] . Coats, T. W. , Harris, C. E. , Lo, D. C. , 1998

机译：叠层复合材料（pDaLC）的渐进损伤分析（Nasa COmET有限元编码实现的计算模型）

A progressive damage fatigue model for unidirectional laminated composites based on Finite Element Analysis: Theory and Practice

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