| 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 conferenceObject |
| URI: | http://hdl.handle.net/11025/30839 https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf |
| 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 |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Straka_P.pdf | Plný text | 436,73 kB | Adobe PDF | View/Open |
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