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 aircooled 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:

    Bestimmung des Kuehlbedarfs eines installierten Motors durch Flugversuch


    Beteiligte:
    Miley, S.J. (Autor:in) / Ward, D.T. (Autor:in) / Kelley, M.N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    9 Seiten, 14 Bilder, 25 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Determination of Installed Reciprocating Engine Cooling Requirements Through Flight Test

    Ward, Donald T. / Kelley, Michael N. / Miley, Stan J. | SAE Technical Papers | 1983


    Flight test method for the determination of reciprocating engine cooling requirements

    Miley, S. J. / Cross, E. J., Jr. / Lawrence, D. L. | NTRS | 1981