Flowfield Around Ogive/Elliptic-Tip Cylinder at High Angle of Attack
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.286
Reference27 articles.
1. Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack
2. Keener, E. R., Chapman, G. T., and Kruse, R. L. “Effects of Mach Number and Afterbody Length on Onset of Asymmetric Forces on Bodies at Zero Sideslip and High Angle of Attack,” AIAA Paper 76-66, Jan. 1976.
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