Influence of forebody cross-sectional shape on wing vortex-burst location
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45490
Reference20 articles.
1. Future fighter technologies
2. Asymmetric vortex forces and wakes on slender bodies
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1. Interactions of Asymmetric Vortices Over Chined Forebody/Wing Configuration at High Angles of Attack;Procedia Engineering;2013
2. Tip-Disturbance Effects on Asymmetric Vortex Breakdown Around a Chined Forebody;Journal of Aircraft;2008-07
3. Effect of Fuselage Cross Sections on Aerodynamic Characteristics of Reusable Launch Vehicles in Subsonic Flow;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007
4. Effects of wings and tunnel walls on forebody vortex asymmetry;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12
5. Aircraft control using stagnation point displacement;1997 World Aviation Congress;1997-08-22
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