A ground vibration test was conducted on a Lockheed JetStar airplane that had been modified for the purpose of conducting laminar flow control experiments. The test was performed prior to initial flight flutter tests. Both sine-dwell and single-point-random excitation methods were used. The data presented include frequency response functions and a comparison of mode frequencies and mode shapes from both methods.


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    Titel :

    Ground vibration test of the laminar flow control JStar airplane


    Beteiligte:
    Kehoe, M. W. (Autor:in) / Cazier, F. W., Jr. (Autor:in) / Ellison, J. F. (Autor:in)

    Erscheinungsdatum :

    01.10.1985


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Ground Vibration Test of the Laminar Flow Control JetStar Airplane

    M. W. Kehoe / F. W. Cazier / J. F. Ellison | NTIS | 1985




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