Technique consists of measuring response of aeroelastically scaled model in simulated free flight to gust field generated in wind tunnel by oscillating airfoils located upstream of test section; freedom of model in approximation of free flight is provided by two-cable support system; description of airstream oscillator system and model mount system; some results of application to fighter-type model are presented.


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    Titel :

    Wind-tunnel technique for measuring frequency-response functions for gust load analyses


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Gilman, Jr., H. (Autor:in) / Bennett, R.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :