Supersonic flow over a pitching delta wing using surface pressure measurements and numerical simulations
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference33 articles.
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2. Gursul I. Review of unsteady vortex flows over slender delta wings. Journal of Aircraft 2005;42(2):299–319.
3. Rockwell D. Three-dimensional flow structure on delta wings at high angle-of-attack: Experimental concepts issues. Reston: AIAA; 1993. Report No.: AIAA-1993-0550.
4. Visbal MR. Computational and physical aspects of vortex breakdown on delta wings. Reston: AIAA; 1993. Report No.: AIAA-1995-0585.
5. Maltby RL, Engler PB, Keating RFA. Some exploratory measurements of leading-edge vortex positions on a delta wing oscillating in heave. Aeronautical research council, research and memorandum. 1963.
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