Extension to the Myers Model for Calculation of Three-Dimensional Glaze Icing
Author:
Affiliation:
1. School of Astronautics Science and Engineering, Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033212
Reference27 articles.
1. Aircraft icing
2. WilderR. W. “A Theoretical and Experimental Means to Predict Ice Accretion Shapes for Evaluation Aircraft Handling and Performance Characteristics,” AGARD Advisory Rept. 127, Neuilly sur Seine, France, 1977.
3. Investigation of surface water behavior during glaze ice accretion
4. Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed
5. Ice accretion prediction on multi-element airfoils
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