Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach

This article discusses an approach for determining meanline geometric parameters of centrifugal compressor stages given specified performance requirements. This is commonly known as the inverse design approach. The opposite process, that of calculating performance parameters based on geometry input...

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Main Authors: Yuri Biba, Peter Menegay
Format: Article
Language:English
Published: Wiley 2004-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/S1023621X04000089
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author Yuri Biba
Peter Menegay
author_facet Yuri Biba
Peter Menegay
author_sort Yuri Biba
collection DOAJ
description This article discusses an approach for determining meanline geometric parameters of centrifugal compressor stages given specified performance requirements. This is commonly known as the inverse design approach. The opposite process, that of calculating performance parameters based on geometry input is usually called analysis, or direct calculation. An algorithm and computer code implementing the inverse approach is described. As an alternative to commercially available inverse design codes, this tool is intended for exclusive OEM use and calls a trusted database of loss models for individual stage components, such as impellers, guide vanes, diffusers, etc. The algorithm extends applicability of the inverse design code by ensuring energy conservation for any working medium, like imperfect gases. The concept of loss coefficient for rotating impellers is introduced for improved loss modelling. The governing conservation equations for each component of a stage are presented, and then described in terms of an iterative procedure which calculates the required one-dimensional geometry. A graphical user interface which facilitates user input and presentation of results is discussed briefly. The object-oriented nature of the code is highlighted as a platform which easily provides for maintainability and future extensions.
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institution Kabale University
issn 1023-621X
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spelling doaj-art-128c72d297f242eaa242e591ec49ea5b2025-02-03T01:32:29ZengWileyInternational Journal of Rotating Machinery1023-621X2004-01-01101758410.1155/S1023621X04000089Inverse Design of Centrifugal Compressor Stages Using a Meanline ApproachYuri Biba0Peter Menegay1Aero-Thermo Design Group, Olean, New York, USAAero-Thermo Design Group, Olean, New York, USAThis article discusses an approach for determining meanline geometric parameters of centrifugal compressor stages given specified performance requirements. This is commonly known as the inverse design approach. The opposite process, that of calculating performance parameters based on geometry input is usually called analysis, or direct calculation. An algorithm and computer code implementing the inverse approach is described. As an alternative to commercially available inverse design codes, this tool is intended for exclusive OEM use and calls a trusted database of loss models for individual stage components, such as impellers, guide vanes, diffusers, etc. The algorithm extends applicability of the inverse design code by ensuring energy conservation for any working medium, like imperfect gases. The concept of loss coefficient for rotating impellers is introduced for improved loss modelling. The governing conservation equations for each component of a stage are presented, and then described in terms of an iterative procedure which calculates the required one-dimensional geometry. A graphical user interface which facilitates user input and presentation of results is discussed briefly. The object-oriented nature of the code is highlighted as a platform which easily provides for maintainability and future extensions.http://dx.doi.org/10.1155/S1023621X04000089
spellingShingle Yuri Biba
Peter Menegay
Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach
International Journal of Rotating Machinery
title Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach
title_full Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach
title_fullStr Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach
title_full_unstemmed Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach
title_short Inverse Design of Centrifugal Compressor Stages Using a Meanline Approach
title_sort inverse design of centrifugal compressor stages using a meanline approach
url http://dx.doi.org/10.1155/S1023621X04000089
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