Thermally Induced Response of Flexible Structures: A Method for Analysis
- 1 January 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance and Control
- Vol. 3 (1) , 92-94
- https://doi.org/10.2514/3.55953
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Thermally Induced Nutational Body Motion of a Spinning Spacecraft with Flexible AppendagesAIAA Journal, 1975
- Thermally induced vibrations of long thin- walled cylinders of open sectionJournal of Spacecraft and Rockets, 1970