Supersonic Axisymmetric Flow over Boattails Containing a Centered Propulsive Jet
Author:
Affiliation:
1. 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/10.2514/3.48576
Reference13 articles.
1. Computation of a Supersonic Flow Past an Axisymmetric Nozzle Boattail with Jet Exhaust
2. Numerical Simulation of Near Wakes Utilizing a Relaxation Turbulence Model
3. 4Sullins, G. A., Anderson, J. D., Jr., and Drummond, J. P. "Numerical Investigation of Supersonic Base Flow with Parallel Injection," AIAA Paper 82-1001,1982.
4. Navier-Stokes Solutions for an Axisymmetric Nozzle
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