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Flow calculation in centrifugal compressors using a quasi-three-dimensional model
When designing centrifugal compressors and turbomachines for various purposes one must carry out the calculation of flow through their fixed and movable elements. One approach to solving this problem is to use the well-proven classical quasi-three-dimensional model. Previously, the authors developed...
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creator | Potashev, A. V. Potasheva, E. V. Hisameev, I. G. |
description | When designing centrifugal compressors and turbomachines for various purposes one must carry out the calculation of flow through their fixed and movable elements. One approach to solving this problem is to use the well-proven classical quasi-three-dimensional model. Previously, the authors developed a method for accounting for the compressibility of a gas stream in the flow part of a turbomachine. This article demonstrates the work of a software package compiled on this basis that performs calculations taking into account the mutual influence of the solutions of two two-dimensional problems in the case of a subsonic gas flow. |
doi_str_mv | 10.1063/5.0026704 |
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V. ; Potasheva, E. V. ; Hisameev, I. G.</creator><contributor>Likholobov, Vladimir A ; Myshlyavtsev, Alexander V ; Yusha, Vladimir L</contributor><creatorcontrib>Potashev, A. V. ; Potasheva, E. V. ; Hisameev, I. G. ; Likholobov, Vladimir A ; Myshlyavtsev, Alexander V ; Yusha, Vladimir L</creatorcontrib><description>When designing centrifugal compressors and turbomachines for various purposes one must carry out the calculation of flow through their fixed and movable elements. One approach to solving this problem is to use the well-proven classical quasi-three-dimensional model. Previously, the authors developed a method for accounting for the compressibility of a gas stream in the flow part of a turbomachine. This article demonstrates the work of a software package compiled on this basis that performs calculations taking into account the mutual influence of the solutions of two two-dimensional problems in the case of a subsonic gas flow.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0026704</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Centrifugal compressors ; Compressibility ; Gas flow ; Gas streams ; Three dimensional models ; Turbomachinery</subject><ispartof>AIP conference proceedings, 2020, Vol.2285 (1)</ispartof><rights>Author(s)</rights><rights>2020 Author(s). 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This article demonstrates the work of a software package compiled on this basis that performs calculations taking into account the mutual influence of the solutions of two two-dimensional problems in the case of a subsonic gas flow.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0026704</doi><tpages>8</tpages></addata></record> |
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identifier | ISSN: 0094-243X |
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language | eng |
recordid | cdi_scitation_primary_10_1063_5_0026704 |
source | American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list) |
subjects | Centrifugal compressors Compressibility Gas flow Gas streams Three dimensional models Turbomachinery |
title | Flow calculation in centrifugal compressors using a quasi-three-dimensional model |
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