Numerical simulation of an F-16A at angle of attack
Author:
Affiliation:
1. Wright Research and Development Center, Wright-Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45953
Reference27 articles.
1. Navier-Stokes solution for a complete re-entry configuration
2. Numerical simulation of the Navier-Stokes equations for an F-16A configuration
3. Calculation of Inviscid Transonic Flow over a Complete Aircraft
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