Divergence study of a high-aspect-ratio, forward swept wing
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Open Access
- 1 May 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (5) , 478-480
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Vortex-airfoil interaction tests1986
- An Automated Procedure for Computing Flutter EigenvaluesJournal of Aircraft, 1974
- Flowfield produced by trailing vortices in the vicinity of the groundAIAA Journal, 1971