Investigation of Transonic and Supersonic Flow in the Blade Cascades Representing Rotor Tip Sections of the Last LP Steam Turbine Stage at Different Turbulence Intensities

0474829 - ÚT 2018 SE eng C - Konferenční příspěvek (zahraniční konf.)
Bobčík, M. - Fořt, J. - Fürst, J. - Halama, J. - Hric, V. - Louda, P. - Luxa, Martin - Rudas, B. - Synáč, J. - Šimurda, David
Investigation of Transonic and Supersonic Flow in the Blade Cascades Representing Rotor Tip Sections of the Last LP Steam Turbine Stage at Different Turbulence Intensities.
Proceedings of 12th European Conference on Turbomachinery Fluid dynamics & Thermodynamics ETC12. Stockholm, 2017, č. článku ETG2017-239..
[European Conference on Turbomachinery Fluid Dynamics and Thermodynamics /12./. Stockholm (SE), 03.04.2017-07.04.2017]
Grant CEP: GA TA ČR(CZ) TA03020277; GA TA ČR(CZ) TH02020057
Institucionální podpora: RVO:61388998
Klíčová slova: steam turbine * transonic flow * tip section * long rotor blade * supersonic flow
Kód oboru RIV: BK - Mechanika tekutin

Design of a new generation of the large power steam turbines leads to very long last rotor blades with tip sections operating often in supersonic region. The flow field in such tip sections is not fully explored and it is believed to be fairly complex and very sensitive even on minute changes of flow parameters. This stimulated the study of the performance of profiles suitable for rotor tip sections. Numerical simulations have been carried out using TU Prague’s code based on the solution of the RANS equations and SST turbulence model by implicit finite volume method with AUSMPW+ scheme in high resolution formulation. Experimental data have been gathered in the intermittent high-speed wind tunnel of IT CAS CR for 2D cascade measurements equipped by an adjustable supersonic inlet nozzle, perforated inserts at side walls and adjustable perforated tailboard.
Trvalý link: http://hdl.handle.net/11104/0279394