Compressible inviscid vortex flow of a sharp edge delta wing
Author:
Affiliation:
1. DLR, German Aerospace Research Establishment, D-38108 Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12631
Reference25 articles.
1. Vortical flow aerodynamics - Physical aspects and numerical simulation
2. Canard-wing vortex interactions at subsonic through supersonic speeds
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