Title: Simulation of supersonic flow through the tip-section turbine blade cascade with a strong shock-wave/boundary-layer interaction
Authors: Straka, P.
Příhoda, J.
Luxa, M.
Citation: Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 123-124.
Issue Date: 2018
Publisher: Západočeská univerzita v Plzni
Document type: konferenční příspěvek
URI: http://hdl.handle.net/11025/30839
ISBN: 978-80-261-0819-1
Keywords: numerická simulace;supersonický proud;lopatky turbíny
Keywords in different language: numerical simulation;supersonic flow;turbine blades
Abstract in different language: Numerical simulations of the supersonic flow have shown the significant effect of the prescription of the outlet boundary condition. Simulations carried out for the standard computational domain with the output behind the blade cascade and/or for the computational domain corresponding to the experimental arrangement have shown that numerical results obtained on the basis of the numerical optimization correspond quite well to experimental data (see Louda et al.). The agreement of predicted flow fields and main parameters including energy losses is acceptable.
Rights: Copyright © 2018 University of West Bohemia, Plzeň, Czech Republic
Appears in Collections:Computational mechanics 2018
Computational mechanics 2018

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