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Proc. ASME. GT2014, Volume 3B: Oil and Gas Applications; Organic Rankine Cycle Power Systems; Supercritical CO2 Power Cycles; Wind Energy, V03BT46A017, June 16–20, 2014

Paper No: GT2014-25920

DOI: https://doi.org/10.1115/GT2014-25920

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Topics: Air jets, Blades, Computational fluid dynamics, Design, Flow (Dynamics), Flow control, Generators, Horizontal axis wind turbines, Maintenance, Navier-Stokes equations

Proceedings Papers

Numerical Study on Three-Dimensional Optimization of a Low-Speed Axial Compressor Rotor

Chenkai Zhang, Jun Hu, Zhiqiang Wang, Chao Yin, Wei Yan

Proc. ASME. GT2014, Volume 2B: Turbomachinery, V02BT45A016, June 16–20, 2014

Paper No: GT2014-26431

DOI: https://doi.org/10.1115/GT2014-26431

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Topics: Compressors, Optimization, Rotors, Flow (Dynamics), Blades, Computer simulation, Design, Engineering prototypes, Flow separation

Journal Articles

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

Chenkai Zhang, Jun Hu, Zhiqiang Wang

J. Eng. Gas Turbines Power. December 2014, 136(12): 122608.

Paper No: GTP-14-1230

DOI: https://doi.org/10.1115/1.4027906

Published Online: July 15, 2014

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Topics: Blades, Boundary layers, Clearances (Engineering), Compressors, Flow (Dynamics), Pressure, Rotors, Design, Inflow, Leakage flows

Journal Articles

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 ]

Chenkai Zhang, Zhiqiang Wang, Chao Yin, Wei Yan, Jun Hu

J. Eng. Gas Turbines Power. December 2014, 136(12): 127001.

Paper No: GTP-14-1252

DOI: https://doi.org/10.1115/1.4027784

Published Online: June 27, 2014

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Topics: Compressors, Gas turbines, High pressure (Physics), Testing

Journal Articles

Low-Speed Model Testing Studies for an Exit Stage of High Pressure Compressor

Chenkai Zhang, Zhiqiang Wang, Chao Yin, Wei Yan, Jun Hu

J. Eng. Gas Turbines Power. November 2014, 136(11): 112603.

Paper No: GTP-14-1204

DOI: https://doi.org/10.1115/1.4027637

Published Online: May 28, 2014

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Topics: Compressors, Flow (Dynamics), Pressure, Rotors, Stators, Design, Blades, Computational fluid dynamics, Testing, Boundary layers

Proceedings Papers

Design Work of a Compressor Stage Through High-to-Low Speed Compressor Transformation

Chenkai Zhang, Jun Hu, Zhiqiang Wang, Xiang Gao

Proc. ASME. GTINDIA2013, ASME 2013 Gas Turbine India Conference, V001T01A001, December 5–6, 2013

Paper No: GTINDIA2013-3506

DOI: https://doi.org/10.1115/GTINDIA2013-3506

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Topics: Compressors, Design, Modeling, Flow (Dynamics), Testing, Blades, Pressure, Aeronautics, Chords (Trusses), Engines

Journal citation

NARROW

Experimental Investigations on Three-Dimensional Blading Optimization for Low-Speed Model Testing

Numerical Study on Tip Leakage Flow Structure of an Axial Flow Compressor Rotor

Study on the Effects of Upstream Flow Conditions and Clearance Sizes to Tip Leakage Flow in a Subsonic Large-Scale Rotor

Numerical Study of Effects of AJVG on Aerodynamic Performance and Speed Control of Small-Scale Fixed-Pitch HAWT

Numerical Study on Three-Dimensional Optimization of a Low-Speed Axial Compressor Rotor

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

Low-Speed Model Testing Studies for an Exit Stage of High Pressure Compressor

Design Work of a Compressor Stage Through High-to-Low Speed Compressor Transformation

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