Method presented which, it is believed, will permit cg range of airplane to be substantially increased, as well as reduce control forces in more satisfactory manner than is customary; method provides cockpit control by which pilot may regulate elevator hinge moment characteristics according to estimate of airplane cg. Before Inst Aeronautical Sciences.


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    Titel :

    New method of longitudinal control for aircraft by use of adjustable angle of attack balance


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    White, R.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1943


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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