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 and rotary wing applications. The NASA program emphasizes technology development in two key areas: advanced ice protection concepts and icing simulation (analytical and experimental). The computer code development/validation, icing wind tunnel testing, and icing flight testing efforts which were conducted to support the icing technology development are reviewed.


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    Title :

    NASA (National Aeronautics and Space Administration) Aircraft Icing Research Program


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

    Publication date :

    1987


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English