Structure of vortex breakdown on a pitching delta wing
Author:
Affiliation:
1. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-434
Reference51 articles.
1. Low speed wind tunnel investigation of the flow about delta wing, oscillating in pitch to very high angle of attack
2. Revnolds. G. and Abtahi. A, "Instabilities in Leading-Edge `Vortex Development," AIAA Paper 87-2424.1987.
3. Measured forces and moments on a delta wing during pitch-up
4. Vortex Breakdown
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1. Numerical modeling of the vortex breakdown phenomenon on a delta wing with trailing-edge jet-flap;International Journal of Heat and Fluid Flow;2010-12
2. Effects of Leading-Edge Radius on Aerodynamic Characteristics of 50º Delta Wings;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
3. Leading-Edge Radius Effects on 50-deg Delta Wing Flow;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
4. Effects of Leading-Edge Shape on the Flow Over 50-deg Delta Wings;26th AIAA Applied Aerodynamics Conference;2008-06-14
5. Vortex Structure on a Delta Wing at High Angle of Attack;AIAA Journal;2002-02
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