Nominal regimes of supersonic profile cascade

0506815 - ÚT 2020 RIV SK eng C - Konferenční příspěvek (zahraniční konf.)
Synáč, J. - Rudas, B. - Luxa, Martin - Fürst, J.
Nominal regimes of supersonic profile cascade.
AIP Conference Proceedings. College Park: American Institute of Physics Inc., 2019 - (Kaduchova, K.; Carnogurska, M.; Lenhard, R.; Brestovic, T.), č. článku 030044. 2118. ISBN 978-073541858-5. ISSN 0094-243X.
[Meeting of Departments of Fluid Mechanics and Thermodynamics /38./. Liptovsky Mikulas (SK), 19.06.2019-21.06.2019]
Grant CEP: GA TA ČR TH02020057
Institucionální podpora: RVO:61388998
Klíčová slova: tip section * long turbine blade * aerodynamic research
Obor OECD: Applied mechanics

This article is concerned with the new design of supersonic profile cascade, marked TR-U-8, for ultra-long bucket tip area. The profile cascade represents a geometrical variant of the ultra-long bucket tip section which was designed in Doosan Skoda Power in Pilsen. There were found out outputs of two aerodynamic regimes marked OP1 India 800 MW for higher back-pressure and OP4 Temelin 1200 MW for lower back pressure. Outputs for nominal incidence cascade angle are presented in this paper. The design of cascades by aerodynamic calculations were investigated and validation by evaluation of optical and pneumatic measurements on wind tunnel tests was done. Two dimensional cascade calculations were carried out by commercial code Ansys Fluent 16.0 in Doosan Škoda Power (DSPW) and by non-commercial software developed in Czech Technical University (CTU). An aerodynamic high speed wind tunnel is located in Institute of Thermomechanics the Czech Academy of Science (AS CR). © 2019 Author(s).
Trvalý link: http://hdl.handle.net/11104/0302642