Spin prediction techniques
Author:
Affiliation:
1. Bihrle Applied Research, Inc., Jericho, New York
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44837
Reference25 articles.
1. Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift
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