Airfoil-Performance-Degradation Prediction Based on Nondimensional Icing Parameters-Reference-Cited by-同舟云学术

Airfoil-Performance-Degradation Prediction Based on Nondimensional Icing Parameters

Published:2013-11 Issue:11 Volume:51 Page:2570-2581
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Han Yiqiang¹,Palacios Jose¹

Affiliation:

1. Department of Aerospace Engineering, Pennsylvania State University, University Park, Pennsylvania 16802

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052207

Reference28 articles.

1. GrayV. “Correlations Among Ice Measurements, Impingement Rates, Icing Conditions, and Drag Coefficients for Unswept NACA 65A004 Airfoil,” NASA TN-4151, 1958.

2. GrayV. H.von GlahnU. H. “Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil,” NACA TN-4155, 1958.

3. FlemmingR. J.LednicerD. A. “High Speed Ice Accretion on Rotorcraft Airfoils,” NASA CR-3910, 1985.

4. An experimental study of airfoil icing characteristics

5. also NASA TM-82790.

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