Design and analysis of dual-constituent lattice sandwich panel with in-plane zero thermal expansion and high structural stiffness
Author:
Affiliation:
1. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian, China
2. Cardiff School of Engineering, Cardiff, UK
Funder
National Science Foundation of China
Program for Changjiang Scholars and Innovative Research Team in University
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/10.1080/15376494.2019.1704099
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1. Design and optimization of an integrated thermal protection system for space vehicles
2. Aerothermodynamic Optimization of Hypersonic Vehicle TPS Design by POD/RSM-Based Approach
3. Design and application of composite platform with extreme low thermal deformation for satellite
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5. Use of glass fibers in tailoring laminated composites with directionally negative and near-zero coefficients of thermal expansion
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