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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Ground Vibration Test of the Laminar Flow Control JetStar Airplane


    Contributors:
    M. W. Kehoe (author) / F. W. Cazier (author) / J. F. Ellison (author)

    Publication date :

    1985


    Size :

    61 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Ground vibration test of the laminar flow control JStar airplane

    Kehoe, M. W. / Cazier, F. W., Jr. / Ellison, J. F. | NTRS | 1985


    Jetstar

    Online Contents | 2007



    The Lockheed JetStar

    Gibson, E. B. | SAE Technical Papers | 1961


    Lockheed jetstar

    Gibson, E.B. | Engineering Index Backfile | 1961