Failure mechanisms of asymmetric sandwich panels subjected to low-velocity impact: An explicit wave dominating damage model-Reference-Cited by-同舟云学术

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Failure mechanisms of asymmetric sandwich panels subjected to low-velocity impact: An explicit wave dominating damage model

Published:2023-11-27 Issue: Volume: Page:1-15
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

Author:

Wu Dake¹,Xiong Xinfa²,Yu Zhangjie³,Peng Ang¹,Deng Jian¹^ORCID,Zhou Guangming¹,Wang Xinwei¹

Affiliation:

1. State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, China

2. AVIC Chengdu Aircraft Design and Research Institute, Chengdu, China

3. Nanjing Engineering Institute of Aircraft Systems, AVIC, Nanjing, China

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation Funded Project

National Key Basic Research and Development Program of China

Fundamental Research Funds for the Central Universities

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15376494.2023.2285410

Reference64 articles.

1. Failure behavior of scarf-bonded woven fabric CFRP laminates

2. Lightweight sandwich structures for marine applications: a review

3. On damage behavior and stability of composite T-shaped stiffened panels under compression after impact considering impact locations

4. Review of composite sandwich structure in aeronautic applications

5. Fabrication and mechanical characterization of CFRP X-core sandwich panels

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1. Numerical study of high-velocity impact on aeronautic carbon composites;Mechanics of Advanced Materials and Structures;2024-07-31

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