Vortex trajectories and breakdown on wing-canard configurations
- 1 August 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (8) , 641-648
- https://doi.org/10.2514/3.45180
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Numerical calculation of nonlinear aerodynamics of wing-body configurationsAIAA Journal, 1983
- On the vortex flow over delta and double-delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Flow studies of slender wing vorticesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Streamwise development of the flow over a delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Spectral characteristics of vortex breakdown flowfieldsPhysics of Fluids, 1979
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971
- A NONLINEAR LIFTING-SURFACE THEORY ESPECIALLY FOR LOWASPECT-RATIO WINGSAIAA Journal, 1963
- Effect of Leading-Edge Separation on the Lift of a Delta WingJournal of the Aeronautical Sciences, 1954