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Journal Articles

Heat Transfer Measurements for Array Jet Impingement With Castellated Wall

Taehyun Kim, Eui Yeop Jung, Minho Bang, Changyong Lee, Hee Koo Moon, Hyung Hee Cho

J. Turbomach. March 2022, 144(3): 031009.

Paper No: TURBO-21-1163

DOI: https://doi.org/10.1115/1.4052315

Published Online: October 5, 2021

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Topics: Flow (Dynamics), Heat, Heat transfer, Impingement cooling, Jets, Mass transfer, Reynolds number, Computational fluid dynamics, Cooling, Gas turbines

Proceedings Papers

Heat Transfer Measurements for Array Jet Impingement With Castellated Wall

Taehyun Kim, Eui Yeop Jung, Minho Bang, Changyong Lee, Hee Koo Moon, Hyung Hee Cho

Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A005, June 7–11, 2021

Paper No: GT2021-58895

DOI: https://doi.org/10.1115/GT2021-58895

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Topics: Heat transfer, Heat, Impingement cooling, Mass transfer, Jets, Pressure, Suction, Combustion chambers, Cooling, Gas turbines

Proceedings Papers

Full Surface Heat Transfer Measurement of a Turbine Internal Cooling System Using a Large Scaled Model

Nojin Park, Changmin Son, Jangsik Yang, Changyong Lee, Kidon Lee

Proc. ASME. GT2018, Volume 5A: Heat Transfer, V05AT16A019, June 11–15, 2018

Paper No: GT2018-77218

DOI: https://doi.org/10.1115/GT2018-77218

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Topics: Cooling systems, Heat transfer, Turbines, Pressure, Flow (Dynamics), Reynolds number, Coolants, Engines, Liquid crystals, Resolution (Optics)

Proceedings Papers

Thermal Performance of the Realistic Leading Edge Cooling Passage of a Turbine Blade

Inhwan Song, Changmin Son, Jangsik Yang, Changyong Lee, Kidon Lee

Proc. ASME. GT2018, Volume 5A: Heat Transfer, V05AT16A018, June 11–15, 2018

Paper No: GT2018-77217

DOI: https://doi.org/10.1115/GT2018-77217

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Topics: Cooling, Turbine blades, Friction, Ducts, Heat transfer, Pressure, Reynolds number, Coolants, Flow (Dynamics), Heat transfer coefficients

Proceedings Papers

Effect of a Gap Between Inner Casing and Stator Blade on Axial Compressor Performance

Changyong Lee, Jaewook Song, Sungryong Lee, Dongmin Hong

Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 203-210, June 14–18, 2010

Paper No: GT2010-22439

DOI: https://doi.org/10.1115/GT2010-22439

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Topics: Blades, Compressors, Stators, Computational fluid dynamics, Corners (Structural elements), Design, Engines, Flow (Dynamics), Gas turbines, Geometric modeling

Journal citation

NARROW

Heat Transfer Measurements for Array Jet Impingement With Castellated Wall

Heat Transfer Measurements for Array Jet Impingement With Castellated Wall

Full Surface Heat Transfer Measurement of a Turbine Internal Cooling System Using a Large Scaled Model

Thermal Performance of the Realistic Leading Edge Cooling Passage of a Turbine Blade

Effect of a Gap Between Inner Casing and Stator Blade on Axial Compressor Performance

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Heat Transfer Measurements for Array Jet Impingement With Castellated Wall

Heat Transfer Measurements for Array Jet Impingement With Castellated Wall

Full Surface Heat Transfer Measurement of a Turbine Internal Cooling System Using a Large Scaled Model

Thermal Performance of the Realistic Leading Edge Cooling Passage of a Turbine Blade

Effect of a Gap Between Inner Casing and Stator Blade on Axial Compressor Performance

Journals

Conference Proceedings

eBooks

Resources

Opportunities

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