Viscous Effects on Missile Aerodynamics at Low Angles of Attack
Author:
Affiliation:
1. Lockheed Missiles & Space Co., Inc., Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57834
Reference32 articles.
1. 4Chapman, G.T. and Keener, E.R. "The Aerodynamics of Bodies of Revolution at Angles of Attack to 90°," AIAA Paper 79-0023, Jan.1979.
2. Vortex-induced asymmetric loads in 2-D and 3-D flows
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