Navier-Stokes computations of the projectile base flow with and without base injection-Reference-Cited by-同舟云学术

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Navier-Stokes computations of the projectile base flow with and without base injection

Published:1983-01-10 Issue: Volume: Page:
ISSN:
Container-title:21st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

SAHU J.¹,NIETUBICZ C.¹,STEGER J.²

Affiliation:

1. U.S. Army, Ballistic Research Laboratories, Aberdeen Proving Ground, MD

2. Stanford University, Palo Alto, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-224

Reference15 articles.

1. Cylindrical and boat-tailed afterbodies in transonic flow with gas ejection

Cited by 10 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. Numerical investigation of supersonic base flow with base speed;20th Atmospheric Flight Mechanics Conference;1995-08-07

2. Application of chimera technique to projectiles in relative motion;Flight Simulation and Technologies;1993-08-09

3. Numerical computations of transonic critical aerodynamic behavior;AIAA Journal;1990-05

4. Theoretical analysis of aircraft afterbody flow;Journal of Spacecraft and Rockets;1987-11

5. Navier-Stokes computations of projectile base flow with and without mass injection;AIAA Journal;1985-09

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