Speed, barometric pressure, and number of revolutions of engine were measured, including tests with stopped engine. Results of gliding tests are used for computation of lift and drag coefficients, and by making use of them, results of engine flights are used for computation of propeller efficiency. (See also Nat. Advisory Committee for Aeronautics Technical Notes no. 92, Apr. 1922 5 pp., 1 fig)


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    Title :

    Full scale determination of the lift and drag of a seaplane


    Additional title:

    Aviation


    Contributors:

    Published in:

    Aviation ; 12 , n 17


    Publication date :

    1922


    Size :

    2 pages


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :