Investigation by NACA to determine performance of small airplane with two Continental A-75 air cooled engines enclosed in wings; one of main problems with engine installations in wing is cooling of engine; steps taken in evolving set of baffles for Continental engine suitable for use in wing of projected airplane and cooling and performance characteristics of engine at sea level and altitude.


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    Title :

    Cooling characteristics of submerged light aircraft engines


    Additional title:

    Soc Automotive Engrs -- Preprint


    Conference:

    Society of Automotive Engineers -- Meeting ; 1941 Cooling



    Publication date :

    1941


    Size :

    10 pages


    Remarks:

    5 Supp sheets


    Type of media :

    Conference Proceedings


    Type of material :

    Print


    Language :

    English




    Cooling Characteristics of SUBMERGED LIGHT AIRCRAFT ENGINES

    ELLERBROCK, H. H. | SAE Technical Papers | 1942


    Cooling characteristics of submerged light aircraft engines

    Ellerbrock, Jr., H.H. | Engineering Index Backfile | 1942


    Liquid cooling of aircraft engines

    Weidinger, H. | Engineering Index Backfile | 1931


    Liquid cooling of aircraft engines

    Weidinger, H. | Engineering Index Backfile | 1931


    Liquid cooling of aircraft engines

    Weidinger, Hanns | TIBKAT | 1931