Navier-Stokes code verification for projectile configurations at supersonic and transonic velocities-Reference-Cited by-同舟云学术

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Navier-Stokes code verification for projectile configurations at supersonic and transonic velocities

Published:1988-05-18 Issue: Volume: Page:
ISSN:
Container-title:15th Aerodynamic Testing Conference
language:
Short-container-title:

Author:

NIETUBICZ C.¹,STUREK W.¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-1995

Reference49 articles.

1. Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow

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

Cited by 3 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. In-pipe aerodynamic characteristics of a projectile in comparison with free flight for transonic Mach numbers;Shock Waves;2018-03-21

2. Investigation of the Magnus Effect of a Generic Projectile at Mach 3 Up to 16 Degrees Angle of Attack;Journal of Applied Mechanics;2013-04-19

3. Recent applications of CFD to the aerodynamics of army projectiles at the U.S. Army Ballistic Research Laboratory;Guidance, Navigation and Control Conference;1992-08-10

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