. "21220" . . . . "9"^^ . "2014-09-24+02:00"^^ . "Modelov\u00E1n\u00ED proud\u011Bn\u00ED ve \u0161pi\u010Dkov\u00E9 turbinov\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei se supersonick\u00FDm vstupem"@cs . "29969" . . . "Modelov\u00E1n\u00ED proud\u011Bn\u00ED ve \u0161pi\u010Dkov\u00E9 turbinov\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei se supersonick\u00FDm vstupem" . "I, P(GAP101/12/1271), P(TA03020277), S" . "The contribution deals with the numerical simulation of compressible flow through the tip-section turbine blade cascade TR-U-4 with supersonic inlet conditions. The prediction is carried out partly by the explicit algebraic model of Reynolds stresses completed by the algebraic transition model and partly by SST turbulence model with the Gamma-Re transition model implemented in Fluent. Obtained results are compared and discussed."@en . . . "1"^^ . "Numerical Simulation; Bypass Transition; Turbine Blade Cascade"@en . "Modelov\u00E1n\u00ED proud\u011Bn\u00ED ve \u0161pi\u010Dkov\u00E9 turbinov\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei se supersonick\u00FDm vstupem"@cs . . "3"^^ . . "Turbostroje 2014" . . "RIV/68407700:21220/14:00226002" . . "Modelling of Flow through the Tip-Section Turbine Blade Cascade with the Supersonic Inlet"@en . "Modelling of Flow through the Tip-Section Turbine Blade Cascade with the Supersonic Inlet"@en . "Straka, P." . "Plze\u0148" . "Plze\u0148" . "Modelov\u00E1n\u00ED proud\u011Bn\u00ED ve \u0161pi\u010Dkov\u00E9 turbinov\u00E9 lopatkov\u00E9 m\u0159\u00ED\u017Ei se supersonick\u00FDm vstupem" . . "RIV/68407700:21220/14:00226002!RIV15-MSM-21220___" . . . "Stod\u016Flka, Ji\u0159\u00ED" . "978-80-260-6447-3" . . . "Z\u00E1pado\u010Desk\u00E1 univerzita v Plzni" . . "[777D397AEFC4]" . "P\u0159\u00EDhoda, J." . "Pr\u00E1ce se zab\u00FDv\u00E1 numerick\u00FDm \u0159e\u0161en\u00EDm stla\u010Diteln\u00E9ho proud\u011Bn\u00ED \u0161pi\u010Dkovou turbinovou m\u0159\u00ED\u017E\u00ED TR-U-4 s nadzvukov\u00FDmi vstupn\u00EDmy okrajov\u00FDmi podm\u00EDnkami. Predikce je \u0159e\u0161ena pomoc\u00ED explicitn\u00EDho algebraick\u00E9ho modelu Reynoldsov\u00FDch nap\u011Bt\u00ED a algebraick\u00FDm modelem p\u0159echodu a rovn\u011B\u017E pomoc\u00ED SST turbulentn\u00EDho modelu s Gamma-Re p\u0159echodem implementovan\u00E1m v softwaru Fluent. Dosa\u017Een\u00E9 v\u00FDsledky jsou porovn\u00E1ny a rozebr\u00E1ny."@cs . "Pr\u00E1ce se zab\u00FDv\u00E1 numerick\u00FDm \u0159e\u0161en\u00EDm stla\u010Diteln\u00E9ho proud\u011Bn\u00ED \u0161pi\u010Dkovou turbinovou m\u0159\u00ED\u017E\u00ED TR-U-4 s nadzvukov\u00FDmi vstupn\u00EDmy okrajov\u00FDmi podm\u00EDnkami. Predikce je \u0159e\u0161ena pomoc\u00ED explicitn\u00EDho algebraick\u00E9ho modelu Reynoldsov\u00FDch nap\u011Bt\u00ED a algebraick\u00FDm modelem p\u0159echodu a rovn\u011B\u017E pomoc\u00ED SST turbulentn\u00EDho modelu s Gamma-Re p\u0159echodem implementovan\u00E1m v softwaru Fluent. Dosa\u017Een\u00E9 v\u00FDsledky jsou porovn\u00E1ny a rozebr\u00E1ny." . .