A flight test procedure has been developed which will provide a systematic means of working cooling installation problems for air-cooled reciprocating engine aircraft. The procedure is based upon the NACA Cooling Correlation analysis which resulted from the radial air-cooled engine development program over forty years ago. The derivation of the method and results from flight test programs to prove the method are reported in this paper.


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    Titel :

    Determination of Installed Reciprocating Engine Cooling Requirements Through Flight Test


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Business Aircraft Meeting and Exposition ; 1983



    Erscheinungsdatum :

    01.02.1983




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch