Restrictor is intended to be applicable to airplanes having stable and reasonably linear pitching-moment characteristics; adjusted results of tests made indicated that acceleration restrictor of type described could limit peak acceleration to about 1.15 times present value by use of proper signal gains and for conditions tested.


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    Title :

    Flight investigation of acceleration restrictor


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    A flight investigation of an acceleration restrictor

    Assadourian, Arthur / Mallick, Donald L. | TIBKAT | 1960


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