Calculation of turbulent flow about missile afterbodies containing an exhaust jet-Reference-Cited by-同舟云学术

Calculation of turbulent flow about missile afterbodies containing an exhaust jet

Published:1984-06-25 Issue: Volume: Page:
ISSN:
Container-title:17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

WAGNER B.¹

Affiliation:

1. Dornier GmbH, Friedrichshafen, West Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1659

Reference21 articles.

1. Eiissiles in Supersonic Flow", AGARD CP-307, 1981 3 HASEN, G.A. "Navier-Stokes Solutions for an

2. Axisynmletric Nozzle", AW-81-147L, 1981 4 DEIWERT, G.S. "A Computational Investigation

3. of Supersonic Axismetric Flow Over Boattails Containing a Centered Propulsive Jet", AIAA-83-0462, 1983 5 FOX, J.H. "Predicting Plume-Induced Separa

4. tion on Bluff Base Bodies", AIAA-84-0315, 1984 6 DEIWERT,G.S. and R O " D , H. "Three-Di

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1. Supersonic base-flow computation using higher-order closure turbulence models;Journal of Spacecraft and Rockets;1996-05

2. Supersonic base flow computation using higher order closure turbulence models;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

3. Computations of supersonic flow over a missile afterbody containing an exhaust jet;Journal of Spacecraft and Rockets;1987-09

4. A method for calculating axisymmetric afterbody flows;Journal of Propulsion and Power;1987-07

5. Accurate numerical simulation of supersonic jet exhaust flow with CSCM on adaptive overlapping grids;25th AIAA Aerospace Sciences Meeting;1987-03-24