Vortex Behaviors of Rolled Supersonic Transport Configuration with Leading-Edge Flaps
Author:
Affiliation:
1. University of Tokyo, Tokyo 113-8656, Japan
2. Japan Aerospace Exploration Agency, Tokyo 181-0015, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.21470
Reference24 articles.
1. The fluid mechanics of slender wing rock
2. Brennenstuhl, U., and Hummel, D. "Vortex Formation over Double-Delta Wings," International Council ofthe Aeronautical Sciences Paper 82-6.6.3,Aug. 1982, pp.1302-1309.
3. Large-amplitude high-rate roll experiments on a delta and double delta wing
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