Aerodynamics of slender rolling wings at incidence in separated flow
- 1 July 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (7) , 886-893
- https://doi.org/10.2514/3.7164
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Effects of Leading-Edge Vortex Flow on the Roll Damping of Slender WingsJournal of Aircraft, 1971
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- A Study of the Flow Field Associated with a Steadily-Rolling Slender Delta WingJournal of the Royal Aeronautical Society, 1964
- Comment on the Stability Derivatives of a Wing-Body-Vertical Tail ConfigurationJournal of the Aeronautical Sciences, 1954