Influence of numerical dissipation in computing supersonic vortex-dominated flows-Reference-Cited by-同舟云学术

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Influence of numerical dissipation in computing supersonic vortex-dominated flows

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

KANDIL O.¹,CHUANG A.¹

Affiliation:

1. Old Dominion University, Norfolk, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1073

Reference30 articles.

1. A nonlinear hybrid vortex method for wings at large angle of attack

2. Paper 55-1552. July 1985. Also to appear i n

3. AIAA Journal, September 1986.

4. 73-89.

Cited by 9 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. Euler Analysis of Forebody-Strake Vortex Flows at Supersonic Speeds;Journal of Aircraft;1993-09

2. Vortex-dominated conical-flow computations using unstructured adaptively-refined meshes;AIAA Journal;1990-11

3. Vertex-based finite-volume solution of the two-dimensional Navier-Stokes equations;AIAA Journal;1990-10

4. Euler solutions for delta wings;AIAA Journal;1990-10

5. Hybrid finite volume approach to Euler solutions for supersonic flows;AIAA Journal;1990-01

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