Investigation of Normal Force Distributions and Wake Vortex Characteristics of Bodies of Revolution at Supersonic Speeds
Author:
Affiliation:
1. McDonnell Aircraft Corporation,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7981
Reference10 articles.
1. First- and Second-Order Theory of Supersonic Flow Past Bodies of Revolution
2. The Estimation of Normal-Force, Drag, and Pitching-Moment Coefficients for Blunt-Based Bodies of Revolution at Large Angles of Attack
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