Rigid-body structural mode coupling on a forward swept wing aircraft
- 1 August 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (8) , 696-702
- https://doi.org/10.2514/3.44931
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Flutter of Asymmetrically Swept WingsAIAA Journal, 1976
- Aerothermoelasticity - Its impact on stability and control of wingedaerospace vehicles.Journal of Aircraft, 1965