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Haokang Jiang
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Proceedings Papers

Experimental Investigation on the Operational Stability of Multistage Centrifugal Compression Systems

Chaoqun Nie, Jingyi Chen, Haokang Jiang
Proc. ASME. GT1999, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A058, June 7–10, 1999
Publisher: American Society of Mechanical Engineers
Paper No: 99-GT-429
https://doi.org/10.1115/99-GT-429
View Paper titled, Experimental Investigation on the Operational Stability of Multistage Centrifugal Compression Systems
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Topics: Compression, Stability, Machinery, Compressors, Cylinders, Oscillations, Pressure, Oxygen, Pressure transducers, Probes
Proceedings Papers

Three-Dimensional Turbulent Flow of the Tip Leakage Vortex in an Axial Compressor Rotor Passage

Hongwei Ma, Haokang Jiang
Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A072, May 8–11, 2000
Publisher: American Society of Mechanical Engineers
Paper No: 2000-GT-0503
https://doi.org/10.1115/2000-GT-0503
View Paper titled, Three-Dimensional Turbulent Flow of the Tip Leakage Vortex in an Axial Compressor Rotor Passage
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Topics: Compressors, Leakage, Rotors, Turbulence, Vortices, Flow (Dynamics), Chords (Trusses), Pressure, Suction, Boundary layers
Proceedings Papers

Three-Dimensional Turbulent Flow Field Downstream of a Single-Stage Axial Compressor Rotor

Hongwei Ma, Haokang Jiang
Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A069, May 8–11, 2000
Publisher: American Society of Mechanical Engineers
Paper No: 2000-GT-0499
https://doi.org/10.1115/2000-GT-0499
View Paper titled, Three-Dimensional Turbulent Flow Field Downstream of a Single-Stage Axial Compressor Rotor
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Topics: Compressors, Rotors, Turbulence, Flow (Dynamics), Chords (Trusses), Corners (Structural elements), Probes, Suction, Wakes, Aerodynamic noise
Proceedings Papers

Three-Dimensional Unsteady Flow Field due to Rotor-Stator Interaction in the Tip Region of an Axial Compressor Stator Passage

Hongwei Ma, Haokang Jiang, Qingguo Zhang
Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A091, June 4–7, 2001
Publisher: American Society of Mechanical Engineers
Paper No: 2001-GT-0597
https://doi.org/10.1115/2001-GT-0597
View Paper titled, Three-Dimensional Unsteady Flow Field due to Rotor-Stator Interaction in the Tip Region of an Axial Compressor Stator Passage
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Topics: Compressors, Rotors, Stators, Unsteady flow, Flow (Dynamics), Vortices, Wakes, Leakage, Fluctuations (Physics), Fluids
Proceedings Papers

Three-Dimensional Turbulent Flow in the Tip Region of an Axial Compressor Rotor Passage at a Near Stall Condition

Hongwei Ma, Haokang Jiang
Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A032, June 4–7, 2001
Publisher: American Society of Mechanical Engineers
Paper No: 2001-GT-0331
https://doi.org/10.1115/2001-GT-0331
View Paper titled, Three-Dimensional Turbulent Flow in the Tip Region of an Axial Compressor Rotor Passage at a Near Stall Condition
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Topics: Compressors, Rotors, Turbulence, Vortices, Chords (Trusses), Corners (Structural elements), Flow (Dynamics), Leakage, Axial flow, Flow separation
Proceedings Papers

Visualizations of the Unsteady Flow Field Near the Endwall of a Compressor Cascade

Hongwei Ma, Haokang Jiang, Lin Yang
Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A033, June 4–7, 2001
Publisher: American Society of Mechanical Engineers
Paper No: 2001-GT-0332
https://doi.org/10.1115/2001-GT-0332
View Paper titled, Visualizations of the Unsteady Flow Field Near the Endwall of a Compressor Cascade
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Topics: Cascades (Fluid dynamics), Compressors, Unsteady flow, Visualization, Flow (Dynamics), Vortices, Bubbles, Hydrogen, Wire, Boundary layers
Proceedings Papers

Three-Dimensional Unsteady Flow Field due to IGV-Rotor Interaction in the Tip Region of an Axial Compressor Rotor Passage

Hongwei Ma, Haokang Jiang, Qingguo Zhang
Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A001, June 4–7, 2001
Publisher: American Society of Mechanical Engineers
Paper No: 2001-GT-0296
https://doi.org/10.1115/2001-GT-0296
View Paper titled, Three-Dimensional Unsteady Flow Field due to IGV-Rotor Interaction in the Tip Region of an Axial Compressor Rotor Passage
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Topics: Compressors, Inlet guide vanes, Rotors, Unsteady flow, Flow (Dynamics), Fluids, Wakes, Corners (Structural elements), Laser Doppler anemometry, Leakage
Proceedings Papers

Visualizations of the Unsteady Flow Field Near the Endwall of a Turbine Cascade

Hongwei Ma, Haokang Jiang, Yaxi Qiu
Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 233-240, June 3–6, 2002
Publisher: American Society of Mechanical Engineers
Paper No: GT2002-30350
https://doi.org/10.1115/GT2002-30350
View Paper titled, Visualizations of the Unsteady Flow Field Near the Endwall of a Turbine Cascade
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Topics: Cascades (Fluid dynamics), Turbines, Unsteady flow, Visualization, Vortices, Suction, Flow (Dynamics), Pressure, Boundary layers, Bubbles
Proceedings Papers

Effect of Leading-Edge Geometry on Separation Bubble on a Compressor Blade

Huoxing Liu, Baojie Liu, Ling Li, Haokang Jiang
Proc. ASME. GT2003, Volume 6: Turbo Expo 2003, Parts A and B, 387-395, June 16–19, 2003
Publisher: American Society of Mechanical Engineers
Paper No: GT2003-38217
https://doi.org/10.1115/GT2003-38217
View Paper titled, Effect of Leading-Edge Geometry on Separation Bubble on a Compressor Blade
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Topics: Blades, Bubbles, Compressors, Geometry, Separation (Technology), Flow (Dynamics), Pressure, Boundary layers, Errors, Design
Proceedings Papers

Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With SPIV

Baojie Liu, Hongwei Wang, Huoxing Liu, Hongjun Yu, Haokang Jiang, Maozhang Chen
Proc. ASME. GT2003, Volume 6: Turbo Expo 2003, Parts A and B, 877-888, June 16–19, 2003
Publisher: American Society of Mechanical Engineers
Paper No: GT2003-38185
https://doi.org/10.1115/GT2003-38185
View Paper titled, Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With SPIV
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Topics: Compressors, Rotors, Unsteady flow, Vortices, Corners (Structural elements), Leakage, Design, Blades, Cross-flow, Fluids
Proceedings Papers

Evolution of the Tip Leakage Vortex in an Axial Compressor Rotor

Baojie Liu, Xianjun Yu, Hongwei Wang, Huoxing Liu, Haokang Jiang, Maozhang Chen
Proc. ASME. GT2004, Volume 5: Turbo Expo 2004, Parts A and B, 503-514, June 14–17, 2004
Publisher: American Society of Mechanical Engineers
Paper No: GT2004-53703
https://doi.org/10.1115/GT2004-53703
View Paper titled, Evolution of the Tip Leakage Vortex in an Axial Compressor Rotor
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Topics: Compressors, Leakage, Rotors, Vortices, Design, Centrifugal force, Coriolis force, Cross-flow, Particulate matter, Stability
Journal Articles

Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With Stereoscopic Particle Image Velocimetry

Baojie Liu, Hongwei Wang, Huoxing Liu, Hongjun Yu, Haokang Jiang, Maozhang Chen
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2004, 126(3): 360–374.
https://doi.org/10.1115/1.1748367
Published Online: September 3, 2004
View Article titled, Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With Stereoscopic Particle Image Velocimetry
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Topics: Compressors, Corners (Structural elements), Flow (Dynamics), Leakage, Rotors, Suction, Vortices, Vorticity, Blades, Particulate matter