Maximum amount of transverse righting moment at rest provided by auxiliary floats or stub wings compared with minimum righting moment required by certain specifications: adequacy of stability evaluated in terms of pilots' opinions based on which U S Navy specification for seaplanes apparently will provide wing tip float having adequate displacement.


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    Title :

    Comparison of design specifications with actual static transverse stability of 25 seaplanes


    Additional title:

    National Advisory Committee Aeronautics -- Technical Note


    Contributors:


    Publication date :

    1947


    Size :

    12 pages


    Remarks:

    8 Supplementary Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :