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.
Aircraft Ground Vibration Test Instrumentation System
1983
28 pages
Report
No indication
English
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