Comparisons in three-dimensionality in the unsteady flows elicited by straight and swept wings
- 17 August 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Visualization of three-dimensional forced unsteady separated flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Three-dimensional unsteady flow fields elicited by a pitching forward swept wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Visualization of wing tip vortices in unsteady and steady windPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Three-dimensionality in unsteady flow about a wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Three-dimensional effects on a pitching lifting surfacePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Interrelated effects of pitch rate and pivot point on airfoil dynamic stallPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- X-29 forward swept wing aerodynamic overviewPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Dynamic stall experiments on oscillating airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975