"[0DA671FBC844]" . "This paper deals with numerical modelling of the development of the boundary layer in transonic turbine blade cascade. The main attention is paid to studying the influence of the supersonic compression on the boundary layer transition to the turbulence. The limiting Reynolds number at which the transition occurs still in region of the supersonic compression was found."@en . "Prediction of Boundary Layer Transition in Transonic Blade Cascade with Sudden Change of Surface Curvature"@en . . . . "8"^^ . . . "1"^^ . . "XVIII. International Scientific Conference The Application of Experimental and Numerical Methods in Fluid Mechanics and Energy 2012" . . "Prediction of Boundary Layer Transition in Transonic Blade Cascade with Sudden Change of Surface Curvature" . . "\u017Dilina" . . "P(GAP101/10/1329), P(IAA200760801), Z(AV0Z20760514)" . . . "3"^^ . "RIV/61388998:_____/12:00376609!RIV13-AV0-61388998" . . "978-80-554-0516-2" . . "Prediction of Boundary Layer Transition in Transonic Blade Cascade with Sudden Change of Surface Curvature" . "computational fluid dynamics; boundary layer; by pass-transition; turbomachinery"@en . . "Prediction of Boundary Layer Transition in Transonic Blade Cascade with Sudden Change of Surface Curvature"@en . "RIV/61388998:_____/12:00376609" . "2012-04-25+02:00"^^ . "\u0160afa\u0159\u00EDk, P." . . "P\u0159\u00EDhoda, Jarom\u00EDr" . . . "\u017Dilinsk\u00E1 univerzita v \u017Diline" . . . "This paper deals with numerical modelling of the development of the boundary layer in transonic turbine blade cascade. The main attention is paid to studying the influence of the supersonic compression on the boundary layer transition to the turbulence. The limiting Reynolds number at which the transition occurs still in region of the supersonic compression was found." . . "Demanovsk\u00E1 dolina" . "161022" . . "Straka, P." .