Aerodynamics of airfoils with vortex trapped by two spanwise fences
- 1 January 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (1) , 146-153
- https://doi.org/10.2514/3.46467
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Two-fence concept for efficient trapping of vortices on airfoilsJournal of Aircraft, 1992
- Experimental analysis of vortex trapping techniquesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Vortex Induced Lift on Two Dimensional Low Speed WingsStudies in Applied Mathematics, 1984
- Prandtl–Batchelor flow past a flat plate with a forward-facing flapJournal of Fluid Mechanics, 1984
- Effect of leading-edge vortex flaps on aerodynamic performance of delta wingsJournal of Aircraft, 1981
- Development of a Vortex-Lift Design Procedure and Application to a Slender Maneuver-Wing ConfigurationJournal of Aircraft, 1981
- Effectiveness of leading-edge vortex flaps on 60 and 75 degree delta wingsJournal of Aircraft, 1981
- Investigation of Delta Wing Leading-Edge DevicesJournal of Aircraft, 1981
- Lift Enhancement by an Externally Trapped VortexJournal of Aircraft, 1978
- Flow over a Wing with an Attached Free VortexStudies in Applied Mathematics, 1977