VEGA launcher base flow prediction at different supersonic Mach numbers
Author:
Affiliation:
1. CIRA - Centro Italiano Ricerche Aerospaziali, Capua, Italy
2. Fiat Avio S.p.A., Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2302
Reference23 articles.
1. Base drag prediction on missile configurations
2. Numerical simulation of steady supersonic flow over an ogive-cylinder-boattail body
3. 4G.S.Deiwert, "Supersonic AxisymmetricFlow over Boattails Containing a Centered Propulsive Jet", AIAA J., Vol.22,No.10, October 1984
4. Comparison of experiment and computation for a missile base region flowfield with a centered propulsive jet
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