Investigation made at request of Navy Bureau of Aeronautics for determining maximum loads during violent maneuvers; existing loading specifications do not conform satisfactorily to loadings existent in critical conditions; in some cases exceeded; acceleration of 10.5 g. recorded in one maneuver in which pilot suffered severely; limits of physical resistance of pilot to violent maneuvers being approached; Navy specifications for structural design included.


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    Title :

    The pressure distribution over the horizontal and vertical tail surfaces of the f6c-4 pursuit airplane in violent maneuvers


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:
    Rhode, R.V. (author)


    Publication date :

    1929


    Size :

    20 pages


    Remarks:

    29 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :