Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil-Reference-Cited by-同舟云学术

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Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:40th Fluid Dynamics Conference and Exhibit
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Author:

Galbraith Marshall¹,Visbal Miguel²

Affiliation:

1. University of Cincinnati

2. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4737

Reference44 articles.

1. 1Schmitz,F.W.,AerodynamikdesFluges,VerlagCarlLange,Duisburg,1960.

2. 2Eppler,R.,AirfoilDesignandData,SpringerVerlag,ISBN3-540-52505-X,1990.

3. 3Selig,M.S.,Donovan,J.F.,Fraser,D.B.,AirfoilsatLowSpeeds,SoartechTechPublications.H.A.Stokely,VirginiaBeach, VA, USA, 1989.

4. 5Smith, A. M. O., Gamberoni, N. "Transition, Pressure Gradient and Stability Theory," Douglas Aircraft Report ES-26388, 1956.

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