An Automated Method for Determining the Flutter Velocity and the Matched Point
- 1 January 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (1) , 21-27
- https://doi.org/10.2514/3.60316
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Second derivatives of the flutter velocity and the optimization of aircraft structures.AIAA Journal, 1972
- An approximate true damping solution of the flutter equation by determinant iteration.Journal of Aircraft, 1971
- Optimization of complex structures to satisfy flutter requirementsAIAA Journal, 1971