Results of preliminary calculations and subsequent flight tests conducted to determine possible improvements in longitudinal stability of G91 jet aircraft due to installation of pitch-damper; calculated and flight test results were compared and agreement was found to be good.


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    Title :

    Investigation on improvement of longitudinal stability of jet aircraft by use of pitch-damper


    Additional title:

    AGARD -- Report


    Contributors:
    Mautino, R. (author)

    Published in:

    Publication date :

    1961


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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