2000a effect of inlet conditions on endwall secondary flowsExit combustor ow and thermal elds entering downstream stator vane passages in a gas turbine engine are highly nonuniform....
Cold-air performance of free power turbine designed for 112-kilowatt automotive gas-turbine engine 3: effect of stator vane end clearances on performanceAn experimental investigation of a free power turbine designed for a 112-kW, automotive, gas turbine engine was made to determine the penalty in performance due to the stator vane end clearances....
Application of an unstructured navier–stokes code to prediction of adiabatic effectiveness of endwall flush-slot-cooling for a stator vane passage ... The code is applied to prediction of adiabatic effectiveness of endwall flush-slot-cooling for a stator vane passage....
Harmonisation of coolant flow pattern with wake of stator vane to improve sealing effectiveness using a wave-shaped rim seal... To characterise the flow phenomena near the wave-shaped rim seal, a simplified model of the wave-shaped rim seal (Type 1 model), which excludes the rotor blade and stator vane, is analysed and compared with the conventional rim seal....
