CFD Investigation of Unsteady Rotorcraft Airfoil Aerodynamics: MiTEs and Dynamic Stall-Reference-Cited by-同舟云学术

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CFD Investigation of Unsteady Rotorcraft Airfoil Aerodynamics: MiTEs and Dynamic Stall

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Coder James¹,Maughmer Mark¹,Martin Preston²

Affiliation:

1. Pennsylvania State University

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1125

Reference33 articles.

1. Leishman, J. G.,Principles ofHelicopter Aerodynamics, 2nded.,Cambridge University Press, New York, 2006.

2. Hartwich, R. "Parametric Study for the Design of Advanced Rotorcraft Airfoils," M.S. Thesis, Department of Aerospace Engineering,The PennsylvaniaState University,University Park, PA,Dec. 1999.

3. Design of Subsonic Airfoils for High Lift

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