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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Pre-1964 SAE Technical Papers ; 1906



    Publication date :

    1948-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    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