A novel methodology to research the residual compressive mechanical properties of composite stiffened panel after low velocity impact based on quantification damage simulation-Reference-Cited by-同舟云学术

A novel methodology to research the residual compressive mechanical properties of composite stiffened panel after low velocity impact based on quantification damage simulation

Published:2022-07-13 Issue:9 Volume:43 Page:5977-5995
ISSN:0272-8397
Container-title:Polymer Composites
language:en
Short-container-title:Polymer Composites

Author:

Xiao Shan¹²,Wu Shibao¹^ORCID,Xu Zhonghai¹^ORCID,Yang Yusong³,Hu Chunxing¹,Du Shanyi¹

Affiliation:

1. National Key Laboratory of Science and Technology on Advanced Composites in Special Environments Harbin Institute of Technology Harbin China

2. Shenyang Aircraft Design and Research Institute Shenyang China

3. No.1 Military Representative Office of Shenyang Military Representative Bureau of Chinese People's Liberation Army Air Force Armament Department Shenyang China

Funder

National Natural Science Foundation of China

National Basic Research Program of China

Publisher

Wiley

Subject

Materials Chemistry,Polymers and Plastics,General Chemistry,Ceramics and Composites

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.26892

Reference45 articles.

1. Experimental and Numerical Study of Low-Velocity Impact and Tensile after Impact for CFRP Laminates Single-Lap Joints Adhesively Bonded Structure

2. Numerical simulation study of ballistic performance of Al2O3/aramid-carbon hybrid FRP laminate composite structures subject to impact loading