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B. C. Y. Cheong
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Journal Articles

Aerothermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers

D. O. O’Dowd, Q. Zhang, L. He, B. C. Y. Cheong, I. Tibbott
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. January 2013, 135(1): 011041.
Paper No: TURBO-11-1183
https://doi.org/10.1115/1.4006537
Published Online: October 31, 2012
View Article titled, Aerothermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers
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Topics: Blades, Clearances (Engineering), Coolants, Cooling, Engines, Film cooling, Flow (Dynamics), Heat transfer, Pressure, Mach number
Proceedings Papers

Aero-Thermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers

D. O. O’Dowd, Q. Zhang, L. He, B. C. Y. Cheong, I. Tibbott
Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 1235-1246, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-45610
https://doi.org/10.1115/GT2011-45610
View Paper titled, Aero-Thermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers
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Topics: Engines, Reynolds number, Film cooling, Chords (Trusses), Clearances (Engineering), Probes, Blades, Cascades (Fluid dynamics), Coolants, Cooling
Journal Articles

Aerothermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers

D. O. O’Dowd, Q. Zhang, L. He, M. L. G. Oldfield, P. M. Ligrani, B. C. Y. Cheong, I. Tibbott
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041026.
https://doi.org/10.1115/1.4003055
Published Online: April 26, 2011
View Article titled, Aerothermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers
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Topics: Blades, Computational fluid dynamics, Flow (Dynamics), Heat transfer, Pressure, Mach number, Suction, Engines, Cascades (Fluid dynamics)
Journal Articles

Overtip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer

Q. Zhang, D. O. O’Dowd, L. He, A. P. S. Wheeler, P. M. Ligrani, B. C. Y. Cheong
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041001.
https://doi.org/10.1115/1.4002949
Published Online: April 19, 2011
View Article titled, Overtip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer
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Topics: Blades, Flow (Dynamics), Heat transfer, Mach number, Pressure, Shock waves, Shock (Mechanics), Turbine blades, Heat transfer coefficients, Heat flux
Proceedings Papers

Aero-Thermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers

D. O. O’Dowd, Q. Zhang, L. He, M. L. G. Oldfield, P. M. Ligrani, B. C. Y. Cheong, I. Tibbott
Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 357-367, June 14–18, 2010
Publisher: American Society of Mechanical Engineers
Paper No: GT2010-22794
https://doi.org/10.1115/GT2010-22794
View Paper titled, Aero-Thermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers
Open the PDF for Aero-Thermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers in another window
Topics: Blades, Cascades (Fluid dynamics), Computational fluid dynamics, Engines, Flow (Dynamics), Heat transfer, Reynolds number, Shock waves, Test facilities, Thermography