A 0.14-scale dynamically scaled model of the space shuttle orbiter wing was tested in the Langley Research Center 16-Foot Transonic Dynamics Wind Tunnel to determine flutter, buffet, and elevon buzz boundaries. Mach numbers between 0.3 and 1.1 were investigated. Rockwell shuttle model 54-0 was utilized for this investigation. A description of the test procedure, hardware, and results of this test is presented.


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    Titel :

    Results of Flutter Test OS6 Obtained Using the 0.14-Scale Wing/Elevon Model (54-0) in the NASA Larc 16-Foot Transonic Dynamics Wind Tunnel


    Beteiligte:
    C. L. Berthold (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch