Hysteresis of vortex development and breakdown on an oscillating delta wing
Author:
Affiliation:
1. Lehigh University, Bethlehem, Pennsylvania
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9812
Reference5 articles.
1. Unsteady Airfoils
2. The pitching delta wing
3. 5Atta, R. "Flow Structure on a Pitching Delta Wing," Ph.D. Dissertation,Dept. of Mechancial Engineering and Mechanics, Lehigh University, Bethlehem, PA, 1987.
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