Unique high-alpha roll dynamics of a sharp-edged 65 deg delta wing
- 6 January 1992
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Effect of leading-edge cross-sectional geometry on slender wing unsteady aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Large-amplitude high-rate roll experiments on a delta and double delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Analytic prediction of the maximum amplitude of slender wing rockJournal of Aircraft, 1989
- Fluid dynamics of unsteady separated flow. Part II. Lifting surfacesProgress in Aerospace Sciences, 1987
- Fluid dynamics of unsteady separated flow. Part I. Bodies of revolutionProgress in Aerospace Sciences, 1986
- Dynamic support interference in high-alpha testingJournal of Aircraft, 1986
- The fluid mechanics of slender wing rockJournal of Aircraft, 1984
- Self-induced wing rock of slender delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Unsteady Aerodynamics of Slender Delta Wings at Large Angles of AttackJournal of Aircraft, 1975
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971