... and HPC. Change in the performance of a notional turbojet engine with circumferential distortion due to the spool coupling effect is presented. Outlook to combine the two methods is briefly summarized at the end. inlet distortion axial flow compressor body force method parallel compressor engine...

.... With the increase of radial skew angle, the efficiency loss caused by slot CT decreases. Thus, the slots with 75 degrees radial skew angle generate the least peak efficiency loss among five kinds of radial skew angle. axial flow compressor stability casing treatment slots radial skew angle tip leakage...

... Gas Turbine Performance Axial Flow Compressor Axial Flow Turbine Preliminary Design Simulation The design of a small gas turbine in the range of 5 kN thrust / 1.2 MW shaft power is being made in association with industry, aiming at distributed power generation and cogeneration. The gas...

... in this paper deals with the variable inlet guide vane (VIGV) transients and the engine transients. A five stage 5:1 pressure ratio axial-flow compressor, delivering 8.1 kg/s air mass flow at design-point, is the basis for the study. The compressor was designed using computer programs developed at ITA...

... 11 01 2011 This work presents the performance study of a 1 MW gas turbine including the effects of blade cooling and compressor variable geometry. The axial flow compressor, with Variable Inlet Guide Vane (VIGV), was designed for this application and its performance maps synthesized...