Instantaneous Crossflow Topology on a Delta Wing in Presence of Vortex Breakdown
Author:
Affiliation:
1. Lehigh University, Bethlehem, Pennsylvania 18015
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2311
Reference18 articles.
1. Topology of Three-Dimensional Separated Flows
2. A Description of Eddying Motions and Flow Patterns Using Critical-Point Concepts
3. Structure of vortex breakdown on a pitching delta wing
4. Three-dimensional flow structure on delta wings at high angle-of-attack - Experimental concepts and issues
5. Instantaneous topology of the unsteady leading-edge vortex at high angle of attack
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2. Skin Friction Fields and Surface Dye Patterns on Delta Wings in Water Flows;Journal of Fluids Engineering;2015-07-01
3. High-Speed Digital-Particle-Image-Velocimetry Study of Vortex Breakdown;AIAA Journal;2005-03
4. Multifaceted Influence of Fuselage Geometry on Delta-Wing Aerodynamics;Journal of Aircraft;2003-01
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