Application of modified hydrodynamic theory for landing impact of seaplane floats. (Restricted Bul L5F15)


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    Title :

    Theoretical and experimental dynamic loads for prismatic float having angle of dead rise of 22 1/2°


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:
    Mayo, W.L. (author)


    Publication date :

    1945


    Size :

    11 pages


    Remarks:

    4 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :