Navier-Stokes analysis of blunt trailing edge airfoils-Reference-Cited by-同舟云学术

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Navier-Stokes analysis of blunt trailing edge airfoils

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

STANAWAY SHARON¹,MCCROSKEY W.¹,KROO ILAN²

Affiliation:

1. NASA, Ames Research Center; U.S. Army, Aeroflightdynamics Directorate, Moffett Field, CA

2. Stanford University, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-24

Reference13 articles.

1. , 'Wind-TunnelInvestigation of Control SurfaceCharacteristics-The Use of a Beveled TrailingEdgeToReducethe HingeMomentof aControlSurface," NACA Wartime Report L-464, March 1942.

2. Henne, P. A, Greg, R. D. "ANew Airfoil DesignConcept," 89-2201-CP.

3. Drela, M. "IntegralBoundary Layer Formulation for Blunt trailing edges," AIAA 89-2166-CP.

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3. Aerodynamic Analysis of Blunt Trailing Edge Airfoils;Journal of Solar Energy Engineering;2003-11-01

4. Computational Study of the High-Lift A-Airfoil;Journal of Aircraft;2001-07

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