Results of combined flight and ground-based dynamic flight simulator study of handling and riding qualities problems associated with low altitude, high speed flight; wide variations of longitudinal stability and control characteristics, considered representative of current and future strike aircraft, were pilot evaluated; results are presented in terms of iso-opinion and iso-performance boundaries defining desired and required stability and control parameters for low altitude, high speed flight; these acceptance boundaries are significantly different from boundaries defined in Military Specifications. (See also J of Aircraft v 1 n 1 Jan-Feb 1964 p 32-40)


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    Title :

    Low-altitude, high-speed handling and riding qualities


    Additional title:

    AGARD -- Report


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :