Transonic flow modes of an axisymmetric blunt body
Author:
Affiliation:
1. Mississippi State University, Starkville, Mississippi
2. California Institute of Technology, Pasadena, California
3. 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/10.2514/3.10262
Reference7 articles.
1. The Drag Related Flow Field Characteristics of Trucks and Buses
2. Aerodynamic effects of probe-induced flow separation on bluff bodiesat transonic Mach numbers
3. Transonic flow modes of an axisymmetric blunt body
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3. Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6;Journal of Spacecraft and Rockets;2010-01
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