An overview of the NASA ongoing efforts to develop an aircraft icing analysis capability is presented. Discussions are included of the overall and long term objectives of the program as well as current capabilities and limitations of the various computer codes being developed. Descriptions are given of codes being developed to analyze two and three dimensional trajectories of water droplets, airfoil ice accretion, aerodynamic performance degradation of components and complete aircraft configurations, electrothermal deicer, fluid freezing point depressant antideicer and electro-impulse deicer. The need for bench mark and verification data to support the code development is also discussed, and selected results of experimental programs are presented.


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    Titel :

    NASA's Aircraft Icing Analysis Program


    Beteiligte:
    R. J. Shaw (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    NASA's aircraft icing technology program

    Reinmann, John J. | NTRS | 1991


    NASA's Aircraft Icing Technology Program

    J. J. Reinmann | NTIS | 1991


    NASA's Aircraft Icing Technology Program

    J. J. Reinmann | NTIS | 1991