Gradient Optimization of Structural Weight for Specified Flutter Speed
- 1 March 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (3) , 143-147
- https://doi.org/10.2514/3.60339
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Optimization of complex structures to satisfy flutter requirementsAIAA Journal, 1971
- Computer Aided Stabilator Design Including Aeroelastic ConstraintsJournal of Aircraft, 1971
- Optimization of structures to satisfy flutter requirements.AIAA Journal, 1969
- Optimum frequency of structures.AIAA Journal, 1968
- Minimum mass bar for axial vibration at specified natural frequency.AIAA Journal, 1967