Aerodynamic Performance of a Swept Wing with Simulated Ice Shapes-Reference-Cited by-同舟云学术

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Aerodynamic Performance of a Swept Wing with Simulated Ice Shapes

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Papadakis Michael¹,Yeong Hsiung-Wei¹,Wong See-Cheuk¹

Affiliation:

1. Wichita State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-734

Reference78 articles.

1. Ashenden, R., Lindberg, W., and Marwitz, J.D. "Two-dimensional NACA 23012 Airfoil Performance Degradation by Super Cooled Cloud, Drizzle, and Rain Drop Icing," AIAA Paper 96-0870, January

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effects of the gap ratio on the flow field structures and the aerodynamic performance of an airfoil with ridge ice;Experimental Thermal and Fluid Science;2024-10

2. The Application of a Five-Hole Probe Wake-Survey Technique to the Study of Swept Wing Icing Aerodynamics;9th AIAA Atmospheric and Space Environments Conference;2017-06-02

3. Aerodynamics of a Swept Wing with Ice Accretion at Low Reynolds Number;30th AIAA Applied Aerodynamics Conference;2012-06-25

4. Simulations of Separated Flow around an Airfoil with Ice Shape using Hybrid RANS/LES Models;29th AIAA Applied Aerodynamics Conference;2011-06-27

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