A Comparative Study Using CFD to Predict Iced Airfoil Aerodynamics-Reference-Cited by-同舟云学术

A Comparative Study Using CFD to Predict Iced Airfoil Aerodynamics

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Chi X.¹,Li Y.²,Addy H.²,Addy Gene³,Choo Yung³,Shih Tom⁴,Chen H.²

Affiliation:

1. Michigan State University

2. Exa Corporation

3. NASA Glenn Research Center

4. Iowa State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1371

Reference30 articles.

1. Chi, X., Zhu, B., Shih, T.I-P., Slater, J.W., Addy, H.E., and Choo, Y.K. "Computing Aerodynamic Performance of 2D Iced Airfoils: Blocking Topology and Grid Generation," AIAA Paper 2002-0381, January2002.

2. Zhu, B., Chi, X., Shih, T.I-P., and Slater, J.W. "Computing Aerodynamic Performance of 2D Iced Airfoils: Blocking Strategies and Convergence Rate," AIAAPaper2002-3049,June2002.

3. Zhu, B., Chi, X., Shih, T.I-P., Slater, J.W., Addy, H.E., and Choo, Y. "Computing Aerodynamic Performance of 2-D Iced Airfoils with Structured Grids,"AIAAPaper2003-1071,January2003.

4. Chung, J., Choo, Y., Reehorst, A., Potapczuk, and Slater, J. "Navier-Stokes Analysis of the Flowfield Characteristics of an Ice Contaminated Aircraft Wing,"AIAA99-0375.

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