Evaluation of four subcritical response methods for on-line prediction of flutter onset in wind tunnel tests
- 1 October 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (10), 835-840
- https://doi.org/10.2514/3.44951
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- The design, testing and analysis of aeroelastically tailored transonic flutter model wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- An approximate true damping solution of the flutter equation by determinant iteration.Journal of Aircraft, 1971