Tests on model to determine relationship between vertical landing acceleration and flight path angle for seaplanes landing in smooth water; results indicated possible hazards accompanying low altitude high speed landings.


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    Title :

    Variation of hydrodynamic impact of loads with flight-path angle for prismatic float at 0° and -- 3° trim and with 22 1/2° angle of dead rise


    Additional title:

    National Advisory Committee Aeronautics -- Technical Note


    Contributors:


    Publication date :

    1947


    Size :

    7 pages


    Remarks:

    4 Supplementary Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :