Smooth water step landing of seaplane is analyzed by solving Newton's differential equation of motion entailing reasonable limiting assumptions; formulas are developed for maximum acceleration; solution is dependent upon definition of apparent water mass.


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    Title :

    Impact theory for seaplane landings


    Additional title:

    National Advisory Committee Aeronautics -- Technical Note


    Contributors:


    Publication date :

    1947


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :