Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor

The paper presents the results of one of the stages of creating a model of assessing and forecasting the operating characteristics of a transonic compressor due to erosive wear. A numerical model of a transonic compressor stage is constructed and verified to substantiate its applicability in calcula...

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Main Authors: V. L. Blinov, I. S. Zubkov
Format: Article
Language:English
Published: Samara National Research University 2023-05-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/19313/9601
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author V. L. Blinov
I. S. Zubkov
author_facet V. L. Blinov
I. S. Zubkov
author_sort V. L. Blinov
collection DOAJ
description The paper presents the results of one of the stages of creating a model of assessing and forecasting the operating characteristics of a transonic compressor due to erosive wear. A numerical model of a transonic compressor stage is constructed and verified to substantiate its applicability in calculating various degrees of blade erosive wear. The article contains a review of the basic approaches for turbulence simulation, their application area and basic features connected with 3D-flow simulation in turbomachines. The parameters and settings of the numerical model are shown. The CFD-obtained results are presented and compared with the experimental data and results of other researchers. By this comparison the accuracy of the CFD-obtained overall performance and the quality of modeling local processes are determined. Possible ways of improving the models accuracy are also specified.
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spelling doaj.art-b6ff4777157a4d1d8c7072fde7d356342023-06-16T07:59:50ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332023-05-01221516210.18287/2541-7533-2023-22-1-51-628839Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressorV. L. Blinov0I. S. Zubkov1Ural Federal UniversityUral Federal UniversityThe paper presents the results of one of the stages of creating a model of assessing and forecasting the operating characteristics of a transonic compressor due to erosive wear. A numerical model of a transonic compressor stage is constructed and verified to substantiate its applicability in calculating various degrees of blade erosive wear. The article contains a review of the basic approaches for turbulence simulation, their application area and basic features connected with 3D-flow simulation in turbomachines. The parameters and settings of the numerical model are shown. The CFD-obtained results are presented and compared with the experimental data and results of other researchers. By this comparison the accuracy of the CFD-obtained overall performance and the quality of modeling local processes are determined. Possible ways of improving the models accuracy are also specified.https://journals.ssau.ru/vestnik/article/viewFile/19313/9601gas turbine unitaxial compressorblade rowdefectscomputational fluid dynamicsverification
spellingShingle V. L. Blinov
I. S. Zubkov
Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
gas turbine unit
axial compressor
blade row
defects
computational fluid dynamics
verification
title Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
title_full Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
title_fullStr Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
title_full_unstemmed Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
title_short Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor
title_sort verification of a transonic stage cfd model for assessing the erosion wear influence on the operation of the axial compressor
topic gas turbine unit
axial compressor
blade row
defects
computational fluid dynamics
verification
url https://journals.ssau.ru/vestnik/article/viewFile/19313/9601
work_keys_str_mv AT vlblinov verificationofatransonicstagecfdmodelforassessingtheerosionwearinfluenceontheoperationoftheaxialcompressor
AT iszubkov verificationofatransonicstagecfdmodelforassessingtheerosionwearinfluenceontheoperationoftheaxialcompressor