Thermoelastic–Structural Analysis of Space Thin-Walled Beam Under Solar Flux
Author:
Affiliation:
1. Yanshan University, 066004 Qinhuangdao, People’s Republic of China
2. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Science and Technology Research Program in Higher Education of Hebei Province of China
Natural Science Foundation of Hebei Province of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057793
Reference9 articles.
1. Thermally induced bending vibrations of a flexible rolled-up solar array
2. Thermally Induced Vibrations of Spinning Thin-Walled Composite Beam
3. Thermally-induced bending-torsion coupling vibration of large scale space structures
4. Thermally Induced Dynamics of a Spinning Spacecraft with an Axial Flexible Boom
5. Thermal-structural analysis for an attitude maneuvering flexible spacecraft under solar radiation
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