Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration
Author:
Affiliation:
1. Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033305
Reference36 articles.
1. BehrbohmH. “Basic Low Speed Aerodynamics of the Short-Coupled Canard Configuration of Small Aspect Ratio,” Saab TN-60, Linkoping, Sweden, 1965.
2. Navier-Stokes simulation of a close-coupled canard-wing-body configuration
3. Computational Study of Subsonic Flow over a Delta Canard-Wing-Body Configuration
4. Flowfield study of a close-coupled canard configuration
5. Low-speed characteristics for the wing-canard configuration of the International Vortex Flow Experiment
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