Axial Compressor Stall and Surge Prediction by Measurements
The paper deals with experimental investigations and analyses of unsteady pressure distributions in different axial compressors. Based on measurements in a single stage research compressor the influence of increasing aerodynamic load onto the pressure and velocity fluctuations is demonstrated. Detai...
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Format: | Article |
Language: | English |
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Wiley
1999-01-01
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Series: | International Journal of Rotating Machinery |
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Online Access: | http://dx.doi.org/10.1155/S1023621X9900007X |
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author | H. Hönen |
author_facet | H. Hönen |
author_sort | H. Hönen |
collection | DOAJ |
description | The paper deals with experimental investigations and analyses of unsteady pressure distributions in different axial compressors. Based on measurements in a single stage research compressor the influence of increasing aerodynamic load onto the pressure and velocity fluctuations is demonstrated. Detailed measurements in a 14-stage and a 17-stage gas turbine compressor are reported. For both compressors parameters could be found which are clearly influenced by the aerodynamic load. |
format | Article |
id | doaj-art-65c03bb4617545aa88e781b60c5a855e |
institution | Kabale University |
issn | 1023-621X |
language | English |
publishDate | 1999-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Rotating Machinery |
spelling | doaj-art-65c03bb4617545aa88e781b60c5a855e2025-02-03T05:59:57ZengWileyInternational Journal of Rotating Machinery1023-621X1999-01-0152778710.1155/S1023621X9900007XAxial Compressor Stall and Surge Prediction by MeasurementsH. Hönen0Institut Für Strahlantriebe und Turboarbeitsmaschinen, RWTH Aachen (Aachen University of Technology), Aachen 52062, GermanyThe paper deals with experimental investigations and analyses of unsteady pressure distributions in different axial compressors. Based on measurements in a single stage research compressor the influence of increasing aerodynamic load onto the pressure and velocity fluctuations is demonstrated. Detailed measurements in a 14-stage and a 17-stage gas turbine compressor are reported. For both compressors parameters could be found which are clearly influenced by the aerodynamic load.http://dx.doi.org/10.1155/S1023621X9900007XStall and surge monitoringUnsteady pressure measurementsCompressor load analysisLoad parametersNeural nets. |
spellingShingle | H. Hönen Axial Compressor Stall and Surge Prediction by Measurements International Journal of Rotating Machinery Stall and surge monitoring Unsteady pressure measurements Compressor load analysis Load parameters Neural nets. |
title | Axial Compressor Stall and Surge Prediction by Measurements |
title_full | Axial Compressor Stall and Surge Prediction by Measurements |
title_fullStr | Axial Compressor Stall and Surge Prediction by Measurements |
title_full_unstemmed | Axial Compressor Stall and Surge Prediction by Measurements |
title_short | Axial Compressor Stall and Surge Prediction by Measurements |
title_sort | axial compressor stall and surge prediction by measurements |
topic | Stall and surge monitoring Unsteady pressure measurements Compressor load analysis Load parameters Neural nets. |
url | http://dx.doi.org/10.1155/S1023621X9900007X |
work_keys_str_mv | AT hhonen axialcompressorstallandsurgepredictionbymeasurements |