Acceleration restrictor which limits elevator motion of aircraft is analyzed by means of electronic analog computer.


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    Title :

    Theoretical analysis of airplane acceleration restrictor controlled by normal acceleration, pitching acceleration, and pitching velocity


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1954


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :