Aircraft Ground Vibration Test Instrumentation System
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1983
- Accession Number
- ADP002694
Entities
People
- David Banaszak
- Richard Talmadge
Organizations
- Wright Laboratory