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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    Title :

    Flight investigation of automatic gust-alleviation system in transport airplane


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    91 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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