Aeroelastic Optimization of a Panel in High Mach Number Supersonic Flow
- 1 September 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (9), 611-617
- https://doi.org/10.2514/3.59048
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Optimization of structures to satisfy flutter requirements.AIAA Journal, 1969
- Application of aeroelastic constraints in structural optimizationPublished by Springer Nature ,1969