Multistage axial compressor flow field predictions using CFD and throughflow calculations

dc.creator	Banjac, Milan
dc.creator	Petrović, Milan
dc.creator	Wiedermann, Alexander
dc.date.accessioned	2022-09-19T17:58:24Z
dc.date.available	2022-09-19T17:58:24Z
dc.date.issued	2016
dc.identifier.uri	https://machinery.mas.bg.ac.rs/handle/123456789/2393
dc.description.abstract	A comparison between two different methods for aerodynamic calculation of multistage axial compressors is presented. Results obtained using classical 2D through-flow calculations were compared with CFD results for several test cases, including various subsonic and supersonic multistage axial compressors with different geometric configurations and stage operating parameters. Calculated flow fields were compared in terms of overall compressor performances, individual blade row operation parameters and spanwise distributions of different flow variables. Nominal and off-design compressor operating conditions were analyzed and all the results were compared with experimental data. Accuracy, advantages and differences between individual methods are discussed.	en
dc.publisher	American Society of Mechanical Engineers (ASME)
dc.rights	restrictedAccess
dc.source	Proceedings of the ASME Turbo Expo
dc.title	Multistage axial compressor flow field predictions using CFD and throughflow calculations	en
dc.type	conferenceObject
dc.rights.license	ARR
dc.citation.other	2C-2016: -
dc.citation.rank	M33
dc.citation.volume	2C-2016
dc.identifier.doi	10.1115/GT2016-57632
dc.identifier.scopus	2-s2.0-84991702047
dc.type.version	publishedVersion