Experimental and Numerical Optimization of a Wing Leading Edge Hot Air Anti-icing System-Reference-Cited by-同舟云学术

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Experimental and Numerical Optimization of a Wing Leading Edge Hot Air Anti-icing System

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Planquart Philippe¹,Vanden Borre Gwenael²,Buchlin Jean-Marie¹

Affiliation:

1. von Karman Institute for Fluid Dynamics

2. Sonaca SA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1277

Reference9 articles.

1. 1MartinH."Heatandmasstransferbetweenimpinginggasjetsandsolidsurfaces",Adv.Heattransfer,vol13,1977.

2. Aircraft anti-icing and de-icing techniques and modeling

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