Comparison of algebraic turbulence models for afterbody flows with jet exhaust
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. Analytical Services and Materials, Inc., Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference22 articles.
1. Evaluation and Application of VSAERO to a Nonaxisymmetric Afterbody with Thrust Vectoring
2. Three-dimensional flow over a conical afterbody containing a centered propulsive jet - A numerical simulation
3. Navier-Stokes computations of prolate spheroids at angle of attack
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2. Supersonic base-flow computation using higher-order closure turbulence models;Journal of Spacecraft and Rockets;1996-05
3. Supersonic base flow computation using higher order closure turbulence models;34th Aerospace Sciences Meeting and Exhibit;1996-01-15
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