Gust alleviation system designed to improve riding comfort investigated in flight; system is capable of reducing normal accelerations due to gusts by 50 to 60% and of simultaneously reducing pitching velocities normally encountered in gusts by about 40%.


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    Titel :

    Flight investigation of automatic gust-alleviation system in transport airplane


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Hunter, P.A. (Autor:in) / Kraft, Jr., C.C. (Autor:in) / Aford, W.L. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    91 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A flight investigation of an automatic gust-alleviation system in a transport airplane

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