Comparison of LEWICE and GlennICE in the SLD Regime-Reference-Cited by-同舟云学术

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Comparison of LEWICE and GlennICE in the SLD Regime

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Wright William¹,Potapczuk Mark²,Levinson Laurie²

Affiliation:

1. ASRC Aerospace

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-439

Reference87 articles.

1. Potapczuk, M. and Gerhart, P. "Progress in development of a Naviér-Stokes solver for evaluation of iced airfoil performance", AIAA-85-0410.

2. Wright, W. "Transient Two dimensional Heat Transfer Through a Composite Body with Application to Deicing of Aircraft Components",AIAA-88-0358.

3. Wright, W. "Two Dimensional Simulation of Electrothermal Deicing of Aircraft Components" J. Aircraft, V26, #6, June1989,pp.554-562.

4. Potapczuk, M. and Bidwell, C. "Swept wing ice accretion modeling",AIAA-90-0756

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