Self-induced roll oscillations measured on a delta wing/canard configuration
- 1 November 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (11) , 814-819
- https://doi.org/10.2514/3.45386
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Subsonic wing rock of slender delta wingsJournal of Aircraft, 1985
- Theory of wing rockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Flow phenomena causing wing and body rockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- The fluid mechanics of slender wing rockJournal of Aircraft, 1984
- Dynamic load measurements with delta wings undergoing self-induced roll oscillationsJournal of Aircraft, 1984
- Aerodynamic aspects of aircraft dynamics at high angles of attackJournal of Aircraft, 1983
- Wing Rock Due to Aerodynamic HysteresisJournal of Aircraft, 1979
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971