Aerodynamic Analysis of a Generic Fighter Using Delayed Detached-Eddy Simulation
Author:
Affiliation:
1. U.S. Air Force Academy, USAFA, Colorado 80840
2. U.S. Air Force, Eglin Air Force Base, Florida 32542
3. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40955
Reference36 articles.
1. Low-speed experimental study of the vortex flow effects of a fighterforebody having unconventional cross-section
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4. The aerodynamic effects of sideslip on double delta wings
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