Conceptual Fluid/Motion Coupling in the Herbst Supermaneuver
Author:
Affiliation:
1. Institute for Aerospace Research, Ottawa, Ontario K1A 0R6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2185
Reference30 articles.
1. F-14A low altitude high angle of attack simulation and flight test program
2. Moving wall effects in unsteady flow
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