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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    Title :

    Determination of installed reciprocating engine cooling requirements through flight test


    Additional title:

    Bestimmung des Kuehlbedarfs eines installierten Motors durch Flugversuch


    Contributors:
    Miley, S.J. (author) / Ward, D.T. (author) / Kelley, M.N. (author)

    Published in:

    Publication date :

    1983


    Size :

    9 Seiten, 14 Bilder, 25 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    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