A Multistage Compressor Test Facility: Uncertainty Analysis and Preliminary Test Results-Reference-Cited by-同舟云学术

A Multistage Compressor Test Facility: Uncertainty Analysis and Preliminary Test Results

Published:2005-01-01 Issue:1 Volume:127 Page:170-177
ISSN:0742-4795
Container-title:Journal of Engineering for Gas Turbines and Power
language:en
Short-container-title:

Author:

Bettocchi R.¹,Pinelli M.¹,Spina P. R.²

Affiliation:

1. Dip. Di Ingegneria, University of Ferrara, Via Saragat, 1, 44100 Ferrara, Italy

2. DIEM—University of Bologna, Viale del Risorgimento, 2, 40136 Bologna, Italy

Abstract

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.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Link

http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/127/1/170/5614270/170_1.pdf

Reference28 articles.

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2. Aker, G. F., and Saravanamuttoo, H. I. H., 1988, “Predicting Gas Turbine Performance Degradation Due to Compressor Fouling Using Computer Simulation Techniques,” ASME Paper No. 88-GT-206.

3. Seddigh, F., and Saravanamuttoo, H. I. H., 1990, “A Proposed Method for Assessing the Susceptibility of Axial Compressors to Fouling,” ASME Paper No. 90-GT-348.

4. Tabakoff, W., Lakshminarasimha, A. N., and Pasin, M., 1990, “Simulation of Compressor Performance Deterioration Due to Erosion,” ASME J. Turbomach., 112, pp. 78–83.

5. Massardo, A., 1991, “Simulation of Fouled Axial Multistage Compressors,” IMechE Paper No. C423/048.

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