Investigation of loads produced upon wings and tail plane of airplane when pulled out of dive to determine satisfactory means of preventing structural failure under extreme conditions; variations made in gear ratio between elevator and control stick, in total time to pull back, in maximum hand load, and in initial diving speed; danger of failure through rough handling only avoided by limiting control load transmitted to elevators.


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    Title :

    Loads on the main planes and tail of an aeroplane when recovering from a dive


    Additional title:

    Aeronautical Research Committee -- Reports Memoranda


    Contributors:
    Bolas, H. (author) / Allward, G.A. (author)


    Publication date :

    1928


    Size :

    24 pages


    Remarks:

    8 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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