Application of the RNG turbulence model to the simulation of axisymmetric supersonic separated base flows
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc., Dublin, PA
2. Cincinnati, Univ., OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-727
Reference36 articles.
1. Ballard,R. O. "TheAerospike/AeroplugEngine,A technical Development Summary",FinalReport, NASA CR NAS8-37814, 1990.
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