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Determination of the first ply failure load for a cross ply laminate subjected to uniaxial tension through computational micromechanics

机译：通过计算微力学确定单轴拉伸交叉层压板的第一层破坏载荷

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Romanowicz Marek;
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1. Determination of the first ply failure load for a cross ply laminate subjected to uniaxial tension through computational micromechanics [J] . Marek Romanowicz International Journal of Solids and Structures . 2014,第13期

机译：通过计算微力学确定单轴拉伸交叉层压板的第一层破坏载荷
2. Micromechanics analysis of progressive failure in cross-ply carbon fiber/epoxy composite under uniaxial loading [J] . Suparerk Sirivedin, Seog Young Han, Kwan Soo Lee Journal of Mechanical Science and Technology . 2007,第12期

机译：单轴载荷下交叉碳纤维/环氧树脂复合材料渐进破坏的微力学分析
3. Micromechanics analysis of progressive failure in cross-ply carbon fiber/epoxy composite under uniaxial loading [J] . Suparerk Sirivedin, Seog Young Han, Kwan Soo Lee Journal of Mechanical Science and Technology . 2007,第12期

机译：单轴载荷下交叉碳纤维/环氧树脂复合材料渐进破坏的微力学分析
4. First Ply Failure Analysis of Laminated Composite Plates Subjected to Transverse Loading [C] . W.j. Liou International conference on computer aided assessment and control of localized damage . 1992

机译：横向载荷的层压复合板的第一帘布层衰竭分析
5. Micromechanical Failure of Transverse-Plies Laminated Fibrous Composites-Fracture/Manufacture Relation [D] . Hussien, Ahmed Esmat. 2013

机译：横向层合层压纤维复合材料的微机械破坏-断裂/制造关系
6. A Simplified Computational Strategy Focused on Resin Damage to Study Matrix Cracking of The Cross-Ply Laminates Under Uniaxial Tension Load [O] . Liangliang Sun, Jihui Wang, Haixiao Hu, 2019

机译：一种以树脂损伤为中心的简化计算策略以研究单轴拉伸载荷下交叉层压板的基体开裂
7. Failure mechanism under tensile loads in CFRP 0-90º cross-ply laminates containing voids [O] . Lozano Pedrero Carles 2007

机译：CFRP0-90º包含空隙的交叉层压板在拉伸载荷下的破坏机理
8. Crack Development in Cross-Ply Laminates under Uniaxial Tension [R] . Gyekenyesi, A. L. 1996

机译：单轴拉伸下交叉层压板的裂纹发展

Determination of the first ply failure load for a cross ply laminate subjected to uniaxial tension through computational micromechanics

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