Cameron C. Cunningham, 1Lt, USAF, Fan and Compressor Branch, Turbine Engine Division, Wright Laboratory 1996.
This report describes the techniques, equipment, and results from the analysis of the frequency response of the 1/4 inch stainless steel traversing kulite probe used in the Compressor Aero Research Facility. Through the use of a shake table, the experimental response of the probe was found and compared to a theoretical model.
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