Vortex unsteadiness on slender bodies at high incidence
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Inc., Sunnyvale, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25919
Reference29 articles.
1. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream
2. Steady and Unsteady Vortex-Induced Asymmetric Loads on Slender Vehicles
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