Variation of Hydrodynamic Impact Loads with Flight-Path Angle for Prismatic Float at 6° and 9° Trim and 22 1/2° Angle of Dead Rise. (Restricted Bul L5K21)


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    Title :

    Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 6° and 9° trim and 22 1/2° angle of dead rise


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1946


    Size :

    6 pages


    Remarks:

    4 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :