Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithm
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta
2. Lockheed Aeronautical Systems Co., Marietta, GA
3. Lockheed Aeronautical Systems Co., Valencia, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-435
Reference12 articles.
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3. Sankar,N. L. and Y.Tassa, "ReynoldsNumber and CompressibilityEffectsonDynamic Stallofa NACA0012Airfoil,"AIAA Paper 80-0010,1980.
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