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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    Title :

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


    Contributors:

    Conference:

    SAE Business Aircraft Meeting, Century 2 ; 1977 ; Wichita, KS, United States


    Publication date :

    1977-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






    Aerodynamics of horizontally-opposed aircraft engine installations

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


    Aerodynamics of horizontally-opposed aircraft engine installations

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