Three-dimensional Navier-Stokes Calculations of Flow Past Isolated Airfoil Leading Edge Surface Roughness-Reference-Cited by-同舟云学术

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Three-dimensional Navier-Stokes Calculations of Flow Past Isolated Airfoil Leading Edge Surface Roughness

Published:2003-06-23 Issue: Volume: Page:
ISSN:
Container-title:33rd AIAA Fluid Dynamics Conference and Exhibit
language:
Short-container-title:

Author:

Matheis Brian¹,Rothmayer Alric¹,Huebsch Wade²

Affiliation:

1. Iowa State University

2. West Virginia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3725

Reference28 articles.

1. Bhaskaran,R.,1989,"Unsteadyincompressibleviscous flow past stationary, pitching or oscillating airfoil leading edges," PhD Dissertation,Iowa State University, Ames, Iowa, 1996.

2. A Study of Vortical Separation from Three-dimensional Symmetric Bumps

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