Tests of drag due to Wright Whirlwind engine, mounted on cabin-type airplane, made in 20-ft. N.A.C.A. Propeller Research Tunnel; drag obtained with three different types of exhaust stacks; drag due to engine found to be 85 lb. at 100 m.p.h. with individual stacks, and 83 lb. at 100 m.p.h. with each of collector rings.


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    Title :

    The drag of A J-5 air-cooled engine


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Notes


    Contributors:
    Weick, F.E. (author)


    Publication date :

    1928


    Size :

    4 pages


    Remarks:

    5 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English