Optimization of a Supersonic Panel Subject to a Flutter Constraint-A Finite-Element Solution
- 1 March 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (3), 404-405
- https://doi.org/10.2514/3.50478
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flowAIAA Journal, 1970
- Derivatives of eigenvalues and eigenvectorsAIAA Journal, 1970
- Optimization of structures to satisfy flutter requirements.AIAA Journal, 1969
- Finite elements applied to panel flutter.AIAA Journal, 1967
- Design of minimum mass structures with specified natural frequencies.AIAA Journal, 1967
- Method of GradientsPublished by Elsevier ,1962