A research program to investigate the aerodynamics of reciprocating aircraft engine cooling installations is discussed. Current results from a flight test program are presented concerning installation flow measurement methods. The influence of different inlet designs on installation cooling effectiveness and efficiency are described.


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    Titel :

    An Investigation of the Aerodynamics and Cooling of a Horizontally-Opposed Engine Installation


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Cross, E. J. (Autor:in) / Owens, J. K. (Autor:in) / Miley, S. J. (Autor:in)

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1977



    Erscheinungsdatum :

    01.02.1977




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






    Aerodynamics of horizontally-opposed aircraft engine installations

    MILEY, S. / CROSS, JR., E. / LAWRENCE, D. et al. | AIAA | 1977


    Aerodynamics of horizontally-opposed aircraft engine installations

    Miley, S. J. / Cross, E. J., Jr. / Lawrence, D. L. et al. | NTRS | 1977


    Determination of Cooling Air Mass Flow for a Horizontally - Opposed Aircraft Engine Installation#

    Cross, E. J. / Ghomi, N. A. / Bridges, P. D. et al. | SAE Technical Papers | 1979