Steady and Unsteady Vortex-Induced Asymmetric Loads on Slender Vehicles
Author:
Affiliation:
1. Lockheed Missiles and Space Company, 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/10.2514/3.57792
Reference100 articles.
1. Missile Aerodynamics - Past, Present, Future
2. Nonlinearities in missile aerodynamics
3. Chapman, G.T. and Keener, E.R. "The Aerodynamics of Bodies of Revolution at Angles of Attack to 90°," AIAA Paper 79-0023, Jan.1979.
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