Three dimensional base flow calculation for a projectile at transonic velocity-Reference-Cited by-同舟云学术

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Three dimensional base flow calculation for a projectile at transonic velocity

Published:1986-05-12 Issue: Volume: Page:
ISSN:
Container-title:4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference
language:
Short-container-title:

Author:

SAHU J.¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1051

Reference14 articles.

1. Numerical Solution of the Azimuthal-Invariant Thin-Layer Navier-Stokes Equations

2. Numerical Simulation of Three-Dimensional Boattail Afterbody Flowfields

3. Navier-Stokes computations of projectile base flow with and without mass injection

Cited by 6 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. Experimental Determination of the Effect of Rifling Grooves on the Aerodynamics of Small Caliber Projectiles;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2006-06-25

2. Velocity Measurements in a Three-Dimensional Compressible Base Flow;AIAA Journal;2003-05

3. Flow Visualizations and Measurements of a Three-Dimensional Supersonic Separated Flow;AIAA Journal;2001-01

4. Aerodynamic computations for a transonic projectile at angle of attack by total variation diminishing schemes;Journal of Spacecraft and Rockets;1993-05

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

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