A multistage compressor test facility, fully instrumented with a dedicated data acquisition and processing system, has been developed to conduct experimental research work at the University of Ferrara. This paper provides a systematic description of the uncertainty analysis procedures required for compressor testing, including preliminary performance test results, in addition to a brief description of the test facility and its capabilities.
A Multistage Compressor Test Facility: Uncertainty Analysis and Preliminary Test Results
Contributed by the International Gas Turbine Institute (IGTI) of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS for publication in the ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Paper presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Atlanta, GA, June 16–19, 2003, Paper No. 2003-GT-38397. Manuscript received by IGTI, October 2002, final revision, March 2003. Associate Editor: H. R. Simmons.
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Bettocchi , R., Pinelli, M., and Spina, P. R. (February 9, 2005). "A Multistage Compressor Test Facility: Uncertainty Analysis and Preliminary Test Results ." ASME. J. Eng. Gas Turbines Power. January 2005; 127(1): 170–177. https://doi.org/10.1115/1.1787516
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