A bistable pure carbon fiber composite symmetric laminate and its preparation, modeling, and experimental verification
Author:
Affiliation:
1. School of Mechanical Engineering and Automation, Northeastern University, Shenyang, China
2. Key Laboratory of Vibration and Control of Aero-propulsion Systems, Northeastern University, Shenyang, China
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Science Center for Gas Turbine 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/10.1080/15376494.2023.2264847
Reference34 articles.
1. Concepts for morphing airfoil sections using bi-stable laminated composite structures
2. Passive load alleviation aerofoil concept with variable stiffness multi-stable composites
3. A nonlinear spring mechanism incorporating a bistable composite plate for vibration isolation
4. Analytical modeling of a device for vibration isolation and energy harvesting using simply-supported bi-stable hybrid symmetric laminate
5. Piezoelectric energy harvester based on bi-stable hybrid symmetric laminate
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