Temperature effect on the static mode I delamination behavior of aerospace‐grade composite laminates: Experimental and numerical study-Reference-Cited by-同舟云学术

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Temperature effect on the static mode I delamination behavior of aerospace‐grade composite laminates: Experimental and numerical study

Published:2022-07-11 Issue:10 Volume:45 Page:2827-2844
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Eng Mat Struct

Author:

Gong Yu¹²³,Jiang Linfei⁴,Li Linkang²,Ren Sue⁵,Zhao Youxuan²,Wang Ziming²,Hu Ning²⁶

Affiliation:

1. State Key Laboratory of Automotive Simulation and Control Jilin University Changchun China

2. College of Aerospace Engineering Chongqing University Chongqing China

3. State Key Laboratory of Coal Mine Disaster Dynamics and Control Chongqing University Chongqing China

4. School of Civil Engineering Chongqing University Chongqing China

5. AECC Beijing Institute of Aeronautic Materials Beijing China

6. School of Mechanical Engineering Hebei University of Technology Tianjin China

Funder

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Natural Science Foundation of Chongqing

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.13784

Reference75 articles.

1. An XFEM-VCCT coupled approach for modeling mode I fatigue delamination in composite laminates under high cycle loading

2. Environmental effects on mode II fatigue delamination growth in an aerospace grade carbon/epoxy composite

3. Experimental assessment of Fully-Uncoupled Multi-Directional specimens for mode I delamination tests

4. A parametric study on the failure strength of multi-bolt composite repairs with different configurations

5. Failure prediction of irregular arranged multi-bolt composite repair based on finite fracture mechanics model

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3. The over-notched flexure test method for determining the fracture toughness and bridging law of laminates;Engineering Fracture Mechanics;2024-05

4. Numerical modelling of the mode I fracture behavior in composite laminates with significant R-curve effect;Theoretical and Applied Fracture Mechanics;2023-12

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