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NASA NTRS ยท 19940014082

Turbulence modeling in aircraft icing

Abstract

The Icing and Cryogenic Technology Branch develops computational tools which predict ice growth on aircraft surfaces and uses existing CFD technology to evaluate the aerodynamic changes associated with such accretions. Surface roughness, transition location, and laminar, transition, or turbulent convective heat transfer all influence the ice growth process on aircraft surfaces. Turbulence modeling is a critical element within the computational tools used for both ice shape prediction and for performance degradation evaluation.

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BibTeXRIS

Potapczuk, Mark G.. 1993-01-01. Turbulence modeling in aircraft icing. https://ntrs.nasa.gov/citations/19940014082

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