Variation of Hydrodynamic Impact Loads with Flight-Path Angle for Prismatic Float at 3° Trim and With 22 1/2 Angle of Dead Rise. (Restricted Bul L 5A24)


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    Title :

    Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 3° trim and with 22 1/2 angle of dead rise


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1945


    Size :

    5 pages


    Remarks:

    3 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :