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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    Titel :

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


    Weitere Titelangaben:

    Aeronautical Research Committee -- Reports Memoranda


    Beteiligte:
    Bolas, H. (Autor:in) / Allward, G.A. (Autor:in)


    Erscheinungsdatum :

    1928


    Format / Umfang :

    24 pages


    Anmerkungen:

    8 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Tail loads in recovering from vertical dive at terminal velocity

    Case, John / Gates, Sidney B. | TIBKAT | 1922


    The Recovery of an Aeroplane from a High Speed Dive

    Young, A.D. / Neumark, S. | Emerald Group Publishing | 1958


    Aerodynamic Deployable Dive Planes

    TITUS MATTHEW / PETERS BRETT | Europäisches Patentamt | 2023

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