The aerodynamic behavior of liquid-cooled aircraft engine cooling installations is reviewed. Design considerations for inlets, diffusers, and exits are discussed. It is shown that the design of an efficient liquid-cooled installation is a technically difficult problem. This problem should not be underestimated in the development program of liquid-cooled aircraft engines.


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    Titel :

    Aerodynamics of Liquid-Cooled Aircraft Engine Installations


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Miley, S. J. (Autor:in)

    Kongress:

    General Aviation Aircraft Meeting and Exposition ; 1985



    Erscheinungsdatum :

    01.07.1985




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    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