Unsteady vortex dynamics and surface pressure topologies on a finite pitching wing
- 1 July 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (4) , 899-907
- https://doi.org/10.2514/3.46577
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Tip vortex, stall vortex, and separation observations on pitching three-dimensional wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Three-dimensional flow field kinematics near the root of an oscillating wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Controlled three-dimensionality in unsteady separated flows about a sinusoidally oscillating flat platePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Visualizing the Connectivity of Vortex Systems for Pitching WingsJournal of Fluids Engineering, 1989
- Three-dimensional vortex systems of finite wingsJournal of Aircraft, 1988
- Unsteady surface pressure measurements on a pitching rectangular wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Numerical modeling of the vortex/airfoil interactionAIAA Journal, 1987
- Comparisons in three-dimensionality in the unsteady flows elicited by straight and swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Visualization of three-dimensional forced unsteady separated flowPublished 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