Data obtained at N.A.C.A. tank from tests on models of three flying-boat hulls, N.A.C.A. Models 11-A, 16, and 22, used to demonstrate effect of trim angle on water resistance; possibility of using tank data on trim angles as aid in piloting; instrument for use in determining trim angle of seaplanes under way; importance of maintaining best trim angle throughout take-off run.


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    Title :

    Effect of trim angle on take-off performance of flying boat


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1934


    Size :

    15 pages


    Remarks:

    4 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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