A technique for gust load alleviation (GLA) flight testing that will approximate a turbulence-like excitation of the wing has been devised. An artificial excitation is produced by randomly deflecting inboard control surfaces on the wing, thereby producing incremental loads on the wing. This presentation covers the background and development of the flight test technique and analyses performed to date.


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    Titel :

    Flight Test Technique for Evaluation of Gust Load Alleviation Analysis Methodology


    Beteiligte:
    B. Perry (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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