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    Investigations on the Effects of Inflow Condition and Tip Clearance Size to the Performance of a Compressor Rotor 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012:;page 122608
    Author(s): Zhang, Chenkai; Hu, Jun; Wang, Zhiqiang
    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, ...
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    Erratum: “Low Speed Model Testing Studies for an Exit Stage of High Pressure Compressorâ€‌ [ASME Journal of Engineering for Gas Turbines and Power, 2014, 136(11), p. 112603, DOI: 10.1115/1.4027637] 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012:;page 127001
    Author(s): Zhang, Chenkai; Wang, Zhiqiang; Yin, Chao; Yan, Wei; Hu, Jun
    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:
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    Low Speed Model Testing Studies for an Exit Stage of High Pressure Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 011:;page 112603
    Author(s): Zhang, Chenkai; Wang, Zhiqiang; Yin, Chao; Yan, Wei; Hu, Jun
    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 ...
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    Experimental Investigations on Three Dimensional Blading Optimization for Low Speed Model Testing 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 012:;page 122602
    Author(s): Zhang, Chenkai; Hu, Jun; Wang, Zhiqiang; Li, Jun
    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 ...
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    DSpace software copyright © 2002-2015  DuraSpace
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