DATA exist now for the design of heated wings on a fundamental wet-air basis. The design method takes into consideration three factors: All of the water intercepted by a wing which is to be heated only in the leading-edge region must be dispersed by evaporation. The design method provides for determining the heat required and the extent of heated area needed to evaporate the intercepted water.


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    Titel :

    Calculation of Heat Required for WING THERMAL ICE PREVENTION in Specified Icing Conditions


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    NEEL, CARR B. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1948-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Calculation of heat required for wing thermal ice prevention in specified icing conditions

    Neel, Jr., C.B. / Bergrun, N.R. / Jukoff, D. et al. | Engineering Index Backfile | 1947


    The calculation of the heat required for wing thermal ice prevention in specified icing conditions

    Neel, C. B., Jr. / Bergrun, N. R. / Jukoff, D. et al. | NTRS | 1947




    Rotary wing icing

    Mazonson, B.P. | Engineering Index Backfile | 1946