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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    Title :

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


    Additional title:

    J Aeronautical Sciences


    Contributors:
    White, R.J. (author)


    Publication date :

    1943


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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