Failure mechanism and impact resistance of all GFRP Miura-ori with platforms sandwich structure under low-velocity impact experiments
Author:
Affiliation:
1. Key Laboratory of Civil Aviation Aircraft Airworthiness Certification Technology, Civil Aviation University of China, Tianjin, PR China
2. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin, PR China
Funder
the basic scientific research business fee project of central universities is specially supported by Civil Aviation University of China
the National Natural Science Foundation of China Youth Project
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/10.1080/15376494.2023.2215230
Reference42 articles.
1. Design and analysis of a thick Miura-ori folded structure with large negative Poisson’s ratio
2. Modal response of carbon-fiber-reinforced Miura-ori core sandwich panels
3. Parametric linear finite element stress and stability analysis of isotropic and orthotropic self-supporting Miura-ori structures
4. Reconfigurable and Deployable Miura-Ori RA Analysis for Satellite Applications
5. Origami Sunshield Concepts for Space Telescopes
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