The Structural Vibration Branch (FIBG) of the Air Force Wright Aeronautical Laboratories is conducting an in-house Ground Vibration Test (GVT) on a full scale F-16 aircraft located inside FIBG's Vibration Aeroelastic facility at Wright-Patterson AFB OH. To measure 120 accelerometer signals simultaneously as required by the GVT, FIBG has designed and fabricated in-house a complete data acquisition system to measure and condition all the required transducer signals. This paper describes the design, configuration, evaluation and calibration of the GVT instrumentation system.


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    Titel :

    Aircraft Ground Vibration Test Instrumentation System


    Beteiligte:
    R. Talmadge (Autor:in) / D. Banaszak (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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