Aerodynamics of Finned Missiles at High Angle of Attack
Author:
Affiliation:
1. The University of Texas at Austin, Austin, Texas
2. The University of Notre Dame, Notre Dame, Ind.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference13 articles.
1. A theory of the flow past a slender delta wing with leading edge separation
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