Close-coupled canard-wing vortex interaction
Author:
Affiliation:
1. Wright-Patterson Air Force Base, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48231
Reference9 articles.
1. Load Distribution on a Close-Coupled Wing Canard at Transonic Speeds
2. Leading-Edge-Vortex Augmentation in Compressible Flow
3. 5White, R. P. Jr. and Zalay, A. D. "High Lift Generation by the Use of Vortices," RASA/SRL Report 74-12, Rochester Applied Science Associates, Rochester, N.Y., July 1975.
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