A 0.14-scale dynamically scaled model of the space shuttle orbiter vertical tail was tested in a 16-foot transonic dynamic wind tunnel to determine flutter, buffet, and rudder buzz boundaries. Mach numbers between .5 and 1.11 were investigated. Rockwell shuttle model 55-0 was used 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 OS7 Obtained Using the 0.14-Scale Space Shuttle Orbiter Fin/Rudder Model Number 55-0 in the NASA LARC 16-Foot Transonic Dynamics Wind Tunnel


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

    Erscheinungsdatum :

    1977


    Format / Umfang :

    57 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch