Effects of vortex breakdown on longitudinal and lateral-directional aerodynamics of slender wings by the suction analogy
- 9 August 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Recent Studies of Subsonic Vortex Lift Including Parameters Affecting Stable Leading-Edge Vortex FlowJournal of Aircraft, 1977
- Calculation of vortex breakdown locations for flow over delta wingsJournal of Aircraft, 1977
- A Quasi-Vortex-Lattice Method in Thin Wing TheoryJournal of Aircraft, 1974
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Some developments in the theory of vortex breakdownJournal of Fluid Mechanics, 1967