Efficient computation of separating high Reynolds number incompressible flows using vorticity confinement-Reference-Cited by-同舟云学术

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Efficient computation of separating high Reynolds number incompressible flows using vorticity confinement

Published:1999-08-22 Issue: Volume: Page:
ISSN:
Container-title:14th Computational Fluid Dynamics Conference
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Author:

Steinhoff John¹,Yonghu Wenren²,Lesong Wang¹

Affiliation:

1. Tennessee, Univ., Tullahoma

2. Flow Analysis, Inc., Tullahoma, TN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3316

Reference29 articles.

Cited by 7 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. Rotor Wake Computing With Lifting Lines and Vorticity Confinement;27th AIAA Applied Aerodynamics Conference;2009-06-14

2. Vorticity Confinement and Advanced Rendering to Compute and Visualize Complex Flows;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

3. Assessment of the Vorticity Confinement Technique Applied to Rotorcraft Flows;21st AIAA Applied Aerodynamics Conference;2003-06-21

4. Computing Blunt Body Flows on Coarse Grids Using Vorticity Confinement;Journal of Fluids Engineering;2002-12-01

5. Numerical Method for Vorticity Confinement in Compressible Flow;AIAA Journal;2002-10

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