Pitch rate and pitch-axis location effects on vortex breakdown onset
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7913
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference30 articles.
1. 2Jarrah, M.A. "Low-Speed Wind-Tunnel Investigation of Flow About Delta Wings, Oscillating in Pitch to Very High Angle of Attack,'1AIAA Paper 89-0295, Jan. 1989.
2. Instabilities in Leading-Edge Vortex Development
3. Measured forces and moments on a delta wing during pitch-up
4. Control of leading-edge vortices on a delta wing
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