Computations of transonic wind tunnel flows about a fully configuredmodel of aircraft by using multi-domain technique-Reference-Cited by-同舟云学术

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Computations of transonic wind tunnel flows about a fully configuredmodel of aircraft by using multi-domain technique

Published:1993-07-06 Issue: Volume: Page:
ISSN:
Container-title:23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference
language:
Short-container-title:

Author:

TAKAKURA YOKO¹,OGAWA SATORU²,WADA YASUHIRO²

Affiliation:

1. Fujitsu, Ltd., Supercomputer Systems Dept., Chiba, Japan

2. National Aerospace Lab., Tokyo, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3022

Reference19 articles.

1. Turbulence models for 3D transonic viscous flows

2. [Z]"Experimental Data Base for Computer Pro gram Assessment, Report of the Fluid Dynamics Panel Working Group 04," AGARD AR138,1979.

3. Steger,J.L., Dougherty,F.C. and Benek,J.A. "A Chimera Grid Scheme; Advances in Grid Generation, Ghia,K.N. and GhiqU. Eds.ASME FED-5, pp.59-69, 1983.

Cited by 1 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. Unsteady flow computations on a flying projectile within a ballistic range;Computers & Fluids;1998-06

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