National Repository of Grey Literature 2 records found  Search took 0.00 seconds. 
Problematic of instability of supersonic inlet flow field in cascades of tip sections of rotor blades
Luxa, Martin ; Bobčík, M. ; Novák, O. ; Radnic, Tomáš ; Synáč, J. ; Šimurda, David
The paper deals with supersonic flow field instability, which occurs in inlet parts of blade cascades representing tip sections of ultra long rotor turbine blades with supersonic inlet velocities.
Simulation of flow through the tip-section turbine blade cascade for various inlet conditions
Straka, P. ; Příhoda, Jaromír
The contribution deals with the numerical simulation of 2D compressible flow through a tip-section of the turbine blade cascade using the EARSM turbulence model completed by the algebraic transition model. Predictions were carried out at the Reynolds number Re2is = 1.85E+06 for Mach numbers M2is = 1.77 and 1.92. The study was focused on the effect of small changes of flow inlet angle and changes of free-stream turbulence on flow structure in the blade cascade, especially on the shock wave/boundary layer interaction.

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