Account of tests on airplane fitted with SW-1 wooden propeller and Kawasaki Special 800-hp 12-cyl liquid cooled engine; span 27.93 m; length 15.06 m; max speed at sea level 250 or 243 km per hr, depending upon weight range. (In Japanese with brief English abstract.)


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    Title :

    Performance calculations on koken long-range monoplane


    Additional title:

    Tokyo Imperial Univ -- Aeronautical Research Inst -- Report


    Contributors:
    Kimura, H. (author)


    Publication date :

    1938


    Size :

    87 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Japanese




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