Methods for calculating supersonic centrifugal impellers and recommendations for their design by numerical methods
| Authors: Zagvozdkin R.I., Drozdov A.A., Marenina L.N. | Published: 04.05.2026 |
| Published in issue: #5(794)/2026 | |
| Category: Mechanical Engineering and Machine Science | Chapter: Hydraulic Machines, Vacuum, Compressor Technology, Hydraulic and Pneumatic Systems | |
| Keywords: supersonic centrifugal impeller, centrifugal compressor, validation of a numerical method, numerical modeling |
Centrifugal compressors are widely used in various industries, in metallurgy, chemical, oil and gas, aviation and others. The obsolescence of some of the existing compressors and the program of import substitution and development of the aviation industry announced by the President and the Government of the Russian Federation creates an urgent problem with a promising method and methodology for designing centrifugal compressors. To design a centrifugal compressors using the listed methods, it is necessary to correctly configure the boundary conditions of the solver and have a grid model that meets the solver requirements. The article presents a description of the results of similar works and an analysis of these results. To conduct our own study of the selected object, where all the necessary data are available in open sources, its digital and grid model was built and a series of calculations were carried out on various grid models, the analysis of the calculations was performed and its results were presented. The validation of the numerical experimental method was carried out, the error of the numerical experimental method was established.
EDN: TGXMON, https://elibrary/tgxmon
References
[1] He X., Zheng X. Mechanisms of sweep on the performance of transonic centrifugal compressor impellers. Appl. Sci., 2017, vol. 7, no. 10, art. 1081, doi: https://doi.org/10.3390/app7101081
[2] Li Z., Wu Y., Lu X. Performance improvement of a highly loaded transonic centrifugal compressor with tandem impeller and freeform blade configuration. Energies, 2022, vol. 15, no. 24, art. 9283, doi: https://doi.org/10.3390/en15249283
[3] Amarel N., Daneshkhah K., Krain H. et al. Optimization of 6.2:1 pressure ratio centrifugal compressor impeller by 3D inverse design. ASME Turbo Expo, 2011, vol. 7, paper GT2011-46505, pp. 2167–2177, doi: https://doi.org/10.1115/GT2011-46505
[4] AC 6-08 description. kbwiki.ercoftac.org: website. URL: https://www.kbwiki.ercoftac.org/w/index.php/AC_6-08_Description (data obrashcheniya: 14.03.2024).
[5] Eisenlohr G., Dalbert P., Krain H. et al. Analysis of the transonic flow at the inlet of a high pressure ratio centrifugal impeller. ASME International Gas Turbine and Aeroengine Congress and Exhibition, 1998, vol. 1, paper 98-GT-024, V001T01A007, doi: https://doi.org/10.1115/98-GT-024
[6] Eisenlohr G., Krain H., Richter F.A. et al. Investigations of the flow through a high pressure ratio centrifugal impeller. ASME Turbo Expo, 2002, vol. 5, paper GT2002-30394, pp. 649–657, doi: https://doi.org/10.1115/GT2002-30394
[7] Eckert B., Schnell E. Axial- und radialkompressoren. Springer, 1961. 528 p. (Russ. ed.: Osevye i tsentrobezhnye kompressory. Moscow, Mashgiz Publ., 1959. 680 p.)
[8] Rodgers C. Typical performance characteristics of gas turbine radial compressors. J. Eng. Power., 1964, vol. 86, no. 2, pp. 161–170, doi: https://doi.org/10.1115/1.3677568
[9] Kholshchevnikov K.V., Emin O.N., Mitrokhin V.T. Teoriya i raschet aviatsionnykh lopatochnykh mashin [Theory and calculation of aircraft blade machines]. Moscow, Mashinostroenie Publ., 1986. 432 p. (In Russ.).
[10] Elfert M., Weber A., Wittrock D. et al. Experimental and numerical verification of an optimization of a fast rotating high performance radial compressor impeller. J. Turbomach., 2017, vol. 139, no. 10, art. 101007, doi: https://doi.org/10.1115/1.4036357
[11] Ris V.F. Tsentrobezhnye kompressornye mashiny [Centrifugal compressor machines]. Mocow, Leningrad, Mashinostroenie Publ., 1964. 334 p. (In Russ.).
[12] Lohmberg A., Casey M.V., Ammann S. Transonic radial compressor inlet design. Proc. Inst. Mech. Eng. A, 2003, vol. 217, no. 4, pp. 367–374, doi: https://doi.org/10.1243/095765003322315423
[13] Rusch D., Casey M.V. The design space boundaries for high flow capacity centrifugal compressors. J. Turbomach., 2013, vol. 135, no. 3, art. 031035, doi: https://doi.org/10.1115/1.4007548
[14] How to manage uncertainty in CFD: the grid convergence index. cfd.university: website. URL: https://cfd.university/blog/how-to-manage-uncertainty-in-cfd-the-grid-convergence-index (accessed: 25.08.2024)
[15] Matas R., Syka T., Lunacek O. Numerical and experimental modelling of the centrifugal compressor stage – setting the model of impellers with 2D blades. EPJ Web Conf., 2017, vol. 143, art. 02073, doi: https://doi.org/10.1051/epjconf/201714302073