Solution presented for motion of prismatic float of infinite length which is dropped vertically into water at zero trim; lift force, simulating seaplane wing lift, assumed to act on float and to remain constant during impact period; solution determined for values of lift ranging from zero to full wing lift.


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    Title :

    Effect of partial wing lift in seaplane landing impact


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Effect of partial wing lift in seaplane landing impact

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