Ice Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel
Ice Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel
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The design and certification of modern transport airplanes for flight in icing conditions increasing relies on three-dimensional numerical simulation tools for ice accretion prediction. There is currently no publically available, high-quality, ice accretion database upon which to evaluate the performance of icing simulation tools for large-scale swept wings that are representative of modern commercial transport airplanes. The purpose of this presentation is to present the results of a series of icing wind tunnel test campaigns whose aim was to provide an ice accretion database for large-scale, swept wings.
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Ice Accretion Test Results for Three Large-Scale Swept-Wing Models in the NASA Icing Research Tunnel
AIAA Atmospheric and Space (ASE) ; 2016 ; Washington, D.C., United States
2016-06-13
Miscellaneous
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English
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