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


    Additional title:

    Eine Untersuchung der Aerodznamik und der Kuehlung von horizontal und gegenlaeufig angeordneten Flugzeugmotoren


    Contributors:
    Milly, S.J. (author)

    Published in:

    Publication date :

    1977


    Size :

    22 Seiten, 29 Bilder, 6 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English