Influence of Reynolds number on forebody side forces for 3.5-diameter tangent-ogive bodies
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2274
Reference14 articles.
1. 4amont,P. 3.: The Complex Asymmetric Flow Over a 3.5D Ogive Nose and Cylindrical Afterbody at High Angles of Attack. AIAA-82-0053, January 1382.
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