Deals with test made in altitude chamber of Bur. of Standards upon a Bavarian Motor Works engine, having six water-cooled cylinders with bore of 5.90 in., stroke of 7.09 in., and compression ratio of 6.7.


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    Title :

    Performance of B.M.W. 185-horsepower airplane engine


    Additional title:

    Nat. Advisory Committee Aeronautics, Report


    Contributors:


    Publication date :

    1922


    Size :

    10 pages


    Remarks:

    22 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English