Magnus Forces on Spinning Supersonic Cones -Part I: The Boundary Layer
Author:
Affiliation:
1. University of California at Davis, Davis, Calif.
2. Sandia Laboratories, Livermore, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61389
Reference17 articles.
1. A Magnus theory
2. Viscous Flow over Spinning Cones at Angle of Attack
3. Boundary layer studies on a spinning cone
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