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The NASA aircraft icing research programThe objective of the NASA aircraft icing research program is to develop and make available to industry icing technology to support the needs and requirements for all-weather aircraft designs. Research is being done for both fixed wing and rotary wing applications. The NASA program emphasizes technology development in two areas, advanced ice protection concepts and icing simulation. Reviewed here are the computer code development/validation, icing wind tunnel testing, and icing flight testing efforts.
Document ID
19920013291
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shaw, Robert J. (NASA Lewis Research Center Cleveland, OH, United States)
Reinmann, John J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1990
Publication Information
Publication: Aeropropulsion 1987
Subject Category
Aircraft Design, Testing And Performance
Accession Number
92N22534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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