Comparison of experiment and computation for a missile base region flowfield with a centered propulsive jet-Reference-Cited by-同舟云学术

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Comparison of experiment and computation for a missile base region flowfield with a centered propulsive jet

Published:1985-07-16 Issue: Volume: Page:
ISSN:
Container-title:18th Fluid Dynamics and Plasmadynamics and Lasers Conference
language:
Short-container-title:

Author:

PETRIE H.¹,WALKER B.¹

Affiliation:

1. U.S. Army, Missile Laboratory, RedstoneArsenal, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1618

Reference35 articles.

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Detached-Eddy Simulation With Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow;Journal of Fluids Engineering;2002-12-01

2. Base Flow Predictions for a Lightsat Launcher at Supersonic Speeds;Journal of Spacecraft and Rockets;1999-03

3. Velocity and Density Measurements in Supersonic High-Temperature Exhaust Plumes;AIAA Journal;1998-07

4. VEGA launcher base flow prediction at different supersonic Mach numbers;15th Applied Aerodynamics Conference;1997-06-23

5. Investigation of the flow past the ARIANE 5 launcher afterbody;Journal of Spacecraft and Rockets;1994-03

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