Numerical simulation of steady supersonic flow over spinning bodies of revolution
Author:
Affiliation:
1. U.S. Army Ballistic Research Laboratory/ARRADCOM, Aberdeen Proving Ground, Maryland
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8011
Reference19 articles.
1. Computations of Magnus effects for a yawed, spinning body of revolution
2. Viscous flow over a cone at moderate incidence—I
3. Calculation of the Flow on a Cone at High Angle of Attack
4. Computation of supersonic viscous flows over ogive-cylinders at angle of attack
5. Hypersonic Laminar Viscous Flow Past Spinning Cones at Angle of Attack
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