A Model for Predicting Post-Stall Behavior of Axial Compressors

The current paper reports on a new theory developed by modifying the basic Moore-Greitzer model, which can predict the performance of a compression system during the instabilities in more details. The general assumptions such as the compression system layout, the lags in the entrance and exit ducts,...

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Main Authors: M. Shahriyari, H. Khaleghi, M. Heinrich
Format: Article
Language:English
Published: Isfahan University of Technology 2021-01-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:http://jafmonline.net/JournalArchive/download?file_ID=55284&issue_ID=1012
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spelling doaj-56732dab177443928b35888fc5576e942021-01-11T08:24:55ZengIsfahan University of Technology Journal of Applied Fluid Mechanics1735-35722021-01-01143897908.A Model for Predicting Post-Stall Behavior of Axial CompressorsM. Shahriyari0H. Khaleghi1M. Heinrich2Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, IranDepartment of Aerospace Engineering, Amirkabir University of Technology, Tehran, IranInstitute for Mechanics and Fluid Dynamics, Technical University Bergakademie, Freiberg, GermanyThe current paper reports on a new theory developed by modifying the basic Moore-Greitzer model, which can predict the performance of a compression system during the instabilities in more details. The general assumptions such as the compression system layout, the lags in the entrance and exit ducts, the compressor axisymmetric characteristic and the small disturbances are similar to those of Moore-Gereitzer model. However, a second order hysteresis is used in the current work for the pressure rise of the rotor and stator rows. As a result, some new parameters are added to the governing equations, such as the stall cell acceleration ( ), second derivative of the mean axial flow coefficient ( ), second derivative of the disturbance amplitude ( ) and slope of the compressor characteristic curve. This gives the modified model new capabilities, like investigating the transient speed of the stall cell or the effect of the throttling rate on the instabilities, which are discussed in details in the current paper.http://jafmonline.net/JournalArchive/download?file_ID=55284&issue_ID=1012surge; rotating stall; compressor characteristic.
collection DOAJ
language English
format Article
sources DOAJ
author M. Shahriyari
H. Khaleghi
M. Heinrich
spellingShingle M. Shahriyari
H. Khaleghi
M. Heinrich
A Model for Predicting Post-Stall Behavior of Axial Compressors
Journal of Applied Fluid Mechanics
surge; rotating stall; compressor characteristic.
author_facet M. Shahriyari
H. Khaleghi
M. Heinrich
author_sort M. Shahriyari
title A Model for Predicting Post-Stall Behavior of Axial Compressors
title_short A Model for Predicting Post-Stall Behavior of Axial Compressors
title_full A Model for Predicting Post-Stall Behavior of Axial Compressors
title_fullStr A Model for Predicting Post-Stall Behavior of Axial Compressors
title_full_unstemmed A Model for Predicting Post-Stall Behavior of Axial Compressors
title_sort model for predicting post-stall behavior of axial compressors
publisher Isfahan University of Technology
series Journal of Applied Fluid Mechanics
issn 1735-3572
publishDate 2021-01-01
description The current paper reports on a new theory developed by modifying the basic Moore-Greitzer model, which can predict the performance of a compression system during the instabilities in more details. The general assumptions such as the compression system layout, the lags in the entrance and exit ducts, the compressor axisymmetric characteristic and the small disturbances are similar to those of Moore-Gereitzer model. However, a second order hysteresis is used in the current work for the pressure rise of the rotor and stator rows. As a result, some new parameters are added to the governing equations, such as the stall cell acceleration ( ), second derivative of the mean axial flow coefficient ( ), second derivative of the disturbance amplitude ( ) and slope of the compressor characteristic curve. This gives the modified model new capabilities, like investigating the transient speed of the stall cell or the effect of the throttling rate on the instabilities, which are discussed in details in the current paper.
topic surge; rotating stall; compressor characteristic.
url http://jafmonline.net/JournalArchive/download?file_ID=55284&issue_ID=1012
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