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RISInvestigations on the Effects of Inflow Condition and Tip Clearance Size to the Performance of a Compressor Rotor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: To clearly clarify the effects of different upstream boundary layer thickness and tip clearance size to the detailed tip flow field and flow mechanism, numerical simulations are performed on a subsonic compressor rotor, ...
Erratum: “Low Speed Model Testing Studies for an Exit Stage of High Pressure Compressor†[ASME Journal of Engineering for Gas Turbines and Power, 2014, 136(11), p. 112603, DOI: 10.1115/1.4027637]
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Figures 12 and 13 on page 6 of the original manuscript contain some errors. The correct figures are as follows:
Low Speed Model Testing Studies for an Exit Stage of High Pressure Compressor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper discusses detailed experimental studies of a lowspeed largescale axial compressor, which is typical of an exit stage of HPC. Numerous measuring techniques were performed, and detailed experimental results were ...
Experimental Investigations on Three Dimensional Blading Optimization for Low Speed Model Testing
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Lowspeed model testing (LSMT) plays a key role in advanced multistage highpressure compressor (HPC) design recently, due to this, employing lowspeed largescale compressor to conduct 3D blading design and detailed flow ...