Analytical study of the subsonic wing-rock phenomenon for slender delta wings
- 1 September 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (9) , 805-809
- https://doi.org/10.2514/3.45844
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Application of the Vortex-Lattice Method to High-Angle-of-Attack Subsonic AerodynamicsSAE International Journal of Advances and Current Practices in Mobility, 1985
- Subsonic wing rock of slender delta wingsJournal of Aircraft, 1985
- The fluid mechanics of slender wing rockJournal of Aircraft, 1984
- Dynamic load measurements with delta wings undergoing self-induced roll oscillationsJournal of Aircraft, 1984