The 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.


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    Title :

    NASA Aircraft Icing Research Program


    Contributors:
    R. J. Shaw (author) / J. J. Reinmann (author)

    Publication date :

    1990


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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    Aircraft Icing Research at NASA

    J. J. Reinmann / R. J. Shaw / W. A. Olsen | NTIS | 1982