2018
DOI: 10.1051/matecconf/201824509002
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Ansys CFX numerical study of stages centrifugal compressor with low-flow rate coefficient

Abstract: The article presents results of applying the methods of computational fluid dynamics for model low-flow rate stages of centrifugal compressors with flow rate coefficient F = 0.028. The computational domain of a model centrifugal compressor for CFD-simulation consists of the following elements: inlet chamber, impeller, vaneless diffuser, return channel, outlet chamber, shaft seal labyrinth, front and back shroud leakage. Full-scale experimental studies were conducted to model stage 028 in air at an inlet pressu… Show more

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Cited by 9 publications
(5 citation statements)
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References 8 publications
(7 reference statements)
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“…The study was carried out on a real prototype stage centrifugal compressor, using the software package ANSYS. The calculation involved the detailed spatial computer model use with a grid of discretization [2][3][4][5][6][7][8][9][10][11] necessary for solving this problem, and real gas parameters [12] were used as working fluid, which directly leads to the increase in the results obtained accuracy. The gas composition is shown in Table 1.…”
Section: Methodsmentioning
confidence: 99%
“…The study was carried out on a real prototype stage centrifugal compressor, using the software package ANSYS. The calculation involved the detailed spatial computer model use with a grid of discretization [2][3][4][5][6][7][8][9][10][11] necessary for solving this problem, and real gas parameters [12] were used as working fluid, which directly leads to the increase in the results obtained accuracy. The gas composition is shown in Table 1.…”
Section: Methodsmentioning
confidence: 99%
“…Numerical methods must be verified and validated before being applied [5]. The largest number of works are concentrated on medium-and high-flow stages with 3D impellers, while relatively few works are concentrated on the verification and validation of numerical calculations with experimental data in stages with low-flow coefficients [6][7][8][9][10][11][12][13]. The estimation of the modeling uncertainty for low-flow stages in the available literature is presented in Table 1.…”
Section: Introductionmentioning
confidence: 99%
“…Large uncertainty in [8] is due to unaccounted gaps and seals. The full stages are presented in four works [10][11][12][13]. In [10], an increased uncertainty of more than 10% for the pressure coefficient is obtained, along with up to 3% for the rest.…”
Section: Introductionmentioning
confidence: 99%
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“…Modern commercial packages for modelling the workflow using computational gas dynamics methods are currently limited due to the need to train specialized personnel and the financial costs of acquiring equipment and licenses. Moreover, a number of scientific publications [9,10,11,12,13,14,15,16,17] show the efficiency of using computational methods in the design and study of centrifugal compressors low-flow rate stages. Computational methods are also used in the calculation of such an important phenomenon as surging in centrifugal compressors [18,19].…”
Section: Introductionmentioning
confidence: 99%