FENSAP-ICE: Application of Unsteady CHT to De-Icing Simulations on a Wing with Inter-Cycle Ice Formation-Reference-Cited by-同舟云学术

FENSAP-ICE: Application of Unsteady CHT to De-Icing Simulations on a Wing with Inter-Cycle Ice Formation

Published:2010-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric and Space Environments Conference
language:
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Author:

Reid Thomas¹,Baruzzi Guido¹,Aliaga Cristhian¹,Aubé Martin¹,Habashi Wagdi²

Affiliation:

1. Newmerical Technologies International

2. McGill University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7835

Reference37 articles.

1. 2Sinnett, M. "787 No Bleed Systems: Saving Fuel and Enhancing Operational Efficiencies", Boeing AERO magazine, Quarter 4,2007.

2. 3DeWitt, K.J., Keith, T.J., Chao, D.F. and Masiulaniec, K.C. "Numerical Simulation of Electrothermal De-Icing Systems", AIAA-83-0114,1983.

3. 4Leffel,K.L."ANumericalandExperimentalInvestigationofElectrothermalAircraftDeicing",NASACR-175024,1986.

4. 5Masiulaniec, K.C. "A Numerical Simulation of the Full Two-Dimensional Electrothermal Deicer Pad", Ph.D. Thesis,UniversityofToledo, Toledo, OH, 1987.

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