Search Results | ASME Digital Collection

1-20 of 221

2 3 4 5

Sort by

Sort Order Select

Journal Articles

THERMAL PERFORMANCE OF DOUBLE-SIDED, PARTIAL HEIGHT STRIP FIN ARRAYS IN A HIGH ASPECT RATIO, RECTANGULAR CHANNEL

Nathaniel Tracy, Lesley Wright, Je-Chin Han

J. Turbomach.

Paper No: TURBO-21-1234

DOI: https://doi.org/10.1115/1.4054544

Published Online: May 11, 2022

View Article

Topics: Heat transfer, Strips, Turbochargers, Fins, Friction, Reynolds number, Flow (Dynamics), Film cooling, Heat transfer coefficients, Pressure drop

Journal Articles

Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With Various 45-Deg Rib Orientations

I-Lun Chen, Izzet Sahin, Lesley M. Wright, Je-Chin Han, Robert Krewinkel

J. Thermal Sci. Eng. Appl. September 2022, 14(9): 091009.

Paper No: TSEA-21-1626

DOI: https://doi.org/10.1115/1.4053741

Published Online: March 8, 2022

View Article

Topics: Blades, Cooling, Heat transfer, Pressure, Rotation, Flow (Dynamics), Reynolds number

Journal Articles

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins

Izzet Sahin, I-Lun Chen, Lesley M. Wright, Je-Chin Han, Hongzhou Xu, Michael Fox

J. Turbomach. September 2022, 144(9): 091009.

Paper No: TURBO-21-1239

DOI: https://doi.org/10.1115/1.4053492

Published Online: March 4, 2022

View Article

Topics: Fins, Flow (Dynamics), Heat transfer, Pressure, Rotation, Strips, Reynolds number, Pressure drop

Proceedings Papers

Computation of Discrete-Hole Film Cooling by a Near-Wall Second-Moment Turbulence Closure

Hamn-Ching Chen, Gengsheng Wei, Je-Chin Han

Proc. ASME. IMECE99, Heat Transfer: Volume 1, 219-226, November 14–19, 1999

Paper No: IMECE1999-0988

DOI: https://doi.org/10.1115/IMECE1999-0988

View Paper

Topics: Computation, Film cooling, Turbulence, Fans, Flow (Dynamics), Anisotropy, Coolants, Resolution (Optics), Stress

Proceedings Papers

Effect of Squealer Geometry Arrangement on Gas Turbine Blade Tip Heat Transfer

Gm Salam Azad, Je-Chin Han, Ronald S. Bunker, C. Pang Lee

Proc. ASME. IMECE2001, Heat Transfer: Volume 5 — Computational, Aerospace and Environmental Heat Transfer, 297-305, November 11–16, 2001

Paper No: IMECE2001/HTD-24314

DOI: https://doi.org/10.1115/IMECE2001/HTD-24314

View Paper

Topics: Blades, Gas turbines, Geometry, Heat transfer, Pressure, Suction, Heat transfer coefficients, Cascades (Fluid dynamics), Chords (Trusses), Flow (Dynamics)

Journal Articles

Influence of Coolant Density on Turbine Blade Tip Film Cooling at Transonic Cascade Flow Conditions Using the Pressure-Sensitive Paint Technique

Izhar Ullah, Sulaiman M. Alsaleem, Lesley M. Wright, Chao-Cheng Shiau, Je-Chin Han

J. Thermal Sci. Eng. Appl. July 2022, 14(7): 071008.

Paper No: TSEA-21-1389

DOI: https://doi.org/10.1115/1.4052455

Published Online: October 20, 2021

View Article

Topics: Blades, Coolants, Density, Film cooling, Flow (Dynamics), Pressure, Leakage flows, Leakage, Design

Journal Articles

Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio

I-Lun Chen, Izzet Sahin, Lesley M. Wright, Je-Chin Han, Robert Krewinkel

J. Turbomach. February 2022, 144(2): 021011.

Paper No: TURBO-21-1166

DOI: https://doi.org/10.1115/1.4052317

Published Online: October 1, 2021

View Article

Topics: Blades, Cooling, Design, Flow (Dynamics), Heat transfer, Pressure, Reynolds number, Rotation, Exterior walls

Proceedings Papers

Influence of Coolant Density on Turbine Blade Film Cooling at Transonic Cascade Flow Conditions Using the Pressure Sensitive Paint Technique

Izhar Ullah, Sulaiman M. Alsaleem, Lesley M. Wright, Chao-Cheng Shiau, Je-Chin Han

Proc. ASME. GT2021, Volume 5A: Heat Transfer — Combustors; Film Cooling, V05AT12A015, June 7–11, 2021

Paper No: GT2021-59366

DOI: https://doi.org/10.1115/GT2021-59366

View Paper

Topics: Blades, Coolants, Density, Film cooling, Flow (Dynamics), Leakage, Paints, Pressure, Turbine blades

Proceedings Papers

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full and Partial Height Strip-Fins

Izzet Sahin, I-Lun Chen, Lesley M. Wright, Je-Chin Han, Hongzhou Xu, Michael Fox

Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A004, June 7–11, 2021

Paper No: GT2021-58877

DOI: https://doi.org/10.1115/GT2021-58877

View Paper

Topics: Fins, Heat transfer, Strips, Rotation, Cooling, Pressure drop, Flow (Dynamics), Heat transfer coefficients, Copper, Design

Proceedings Papers

Jet Impingement Heat Transfer in a Rectangular Channel With Smooth and Pinned Target Walls

Yasser S. Alzahrani, Lesley M. Wright, Andrew Chen, Je-Chin Han

Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A010, June 7–11, 2021

Paper No: GT2021-59343

DOI: https://doi.org/10.1115/GT2021-59343

View Paper

Topics: Fins, Heat transfer

Proceedings Papers

Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio

I-Lun Chen, Izzet Sahin, Lesley M. Wright, Je-Chin Han, Robert Krewinkel

Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A012, June 7–11, 2021

Paper No: GT2021-59400

DOI: https://doi.org/10.1115/GT2021-59400

View Paper

Topics: Blades, Cooling, Heat transfer

Proceedings Papers

Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel

Nathaniel J. Tracy, Lesley M. Wright, Je-Chin Han

Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A019, June 7–11, 2021

Paper No: GT2021-59774

DOI: https://doi.org/10.1115/GT2021-59774

View Paper

Topics: Friction, Heat transfer, Strips

Journal Articles

Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations

Sulaiman M. Alsaleem, Lesley M. Wright, Je-Chin Han

J. Turbomach. September 2021, 143(9): 091015.

Paper No: TURBO-20-1382

DOI: https://doi.org/10.1115/1.4050627

Published Online: May 12, 2021

View Article

Topics: Heat transfer, Turning vanes, Pressure, Flow (Dynamics), Reynolds number

Journal Articles

Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs

I-Lun Chen, Izzet Sahin, Lesley M. Wright, Je-Chin Han, Robert Krewinkel

J. Turbomach. August 2021, 143(8): 081013.

Paper No: TURBO-20-1348

DOI: https://doi.org/10.1115/1.4050447

Published Online: May 3, 2021

View Article

Topics: Cooling, Heat transfer, Reynolds number, Rotation, Flow (Dynamics), Pressure

Journal Articles

Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins

Izzet Sahin, I-Lun Chen, Lesley M. Wright, Je-Chin Han, Hongzhou Xu, Michael Fox

J. Turbomach. July 2021, 143(7): 071007.

Paper No: TURBO-20-1294

DOI: https://doi.org/10.1115/1.4050355

Published Online: April 9, 2021

View Article

Topics: Fins, Flow (Dynamics), Heat transfer, Rotation, Pressure, Reynolds number, Cooling

Journal Articles

Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade

Daniel A. Salinas, Izhar Ullah, Lesley M. Wright, Je-Chin Han, John W. McClintic, Daniel C. Crites, Ardeshir Riahi

J. Turbomach. June 2021, 143(6): 061012.

Paper No: TURBO-20-1301

DOI: https://doi.org/10.1115/1.4050357

Published Online: April 9, 2021

View Article

Topics: Cascades (Fluid dynamics), Coolants, Film cooling, Flow (Dynamics), Pressure, Mach number, Density, Cooling

Journal Articles

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins

Izzet Sahin, I-Lun Chen, Lesley M. Wright, Je-Chin Han, Hongzhou Xu, Michael Fox

J. Turbomach. June 2021, 143(6): 061009.

Paper No: TURBO-20-1168

DOI: https://doi.org/10.1115/1.4050241

Published Online: April 8, 2021

View Article

Topics: Fins, Heat transfer, Flow (Dynamics), Pressure, Rotation, Pins (Engineering), Cooling

Journal Articles

Heat Transfer Enhancement in a Rectangular Cooling Channel With Airfoil Shaped Fins

Lesley M. Wright, Andrew F. Chen, Hao-Wei Wu, Je-Chin Han, Ching-Pang Lee, Salam Azad, Jae Um

J. Thermal Sci. Eng. Appl. August 2021, 13(4): 041026.

Paper No: TSEA-20-1248

DOI: https://doi.org/10.1115/1.4049424

Published Online: January 22, 2021

View Article

Topics: Airfoils, Fins, Heat transfer, Heat transfer coefficients, Flow (Dynamics), Cooling, Strips, Temperature, Friction, Pressure

Proceedings Papers

Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Degree Tip Turn With Different Turning Vane Configurations

Sulaiman M. Alsaleem, Lesley M. Wright, Je-Chin Han

Proc. ASME. GT2020, Volume 7A: Heat Transfer, V07AT15A008, September 21–25, 2020

Paper No: GT2020-14510

DOI: https://doi.org/10.1115/GT2020-14510

View Paper

Topics: Heat transfer, Pressure, Turning vanes, Cooling, Flow (Dynamics), Design, Pressure drop, Reynolds number, Blades, Gas turbines

Proceedings Papers

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Smooth Walls and Pin-Fins

Izzet Sahin, I-Lun Chen, Lesley M. Wright, Je-Chin Han, Hongzhou Xu, Michael Fox

Proc. ASME. GT2020, Volume 7A: Heat Transfer, V07AT15A005, September 21–25, 2020

Paper No: GT2020-14440

DOI: https://doi.org/10.1115/GT2020-14440

View Paper

Topics: Fins, Heat transfer, Rotation, Pressure drop, Reynolds number, Cooling, Flow (Dynamics), Heat transfer coefficients, Copper, Geometry

2 3 4 5

Journal citation

NARROW

Manuscript

THERMAL PERFORMANCE OF DOUBLE-SIDED, PARTIAL HEIGHT STRIP FIN ARRAYS IN A HIGH ASPECT RATIO, RECTANGULAR CHANNEL

Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With Various 45-Deg Rib Orientations

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins

Computation of Discrete-Hole Film Cooling by a Near-Wall Second-Moment Turbulence Closure

Effect of Squealer Geometry Arrangement on Gas Turbine Blade Tip Heat Transfer

Influence of Coolant Density on Turbine Blade Tip Film Cooling at Transonic Cascade Flow Conditions Using the Pressure-Sensitive Paint Technique

Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio

Influence of Coolant Density on Turbine Blade Film Cooling at Transonic Cascade Flow Conditions Using the Pressure Sensitive Paint Technique

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full and Partial Height Strip-Fins

Jet Impingement Heat Transfer in a Rectangular Channel With Smooth and Pinned Target Walls

Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio

Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel

Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations

Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs

Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins

Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins

Heat Transfer Enhancement in a Rectangular Cooling Channel With Airfoil Shaped Fins

Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Degree Tip Turn With Different Turning Vane Configurations

Heat Transfer in Rotating, Trailing Edge, Converging Channels With Smooth Walls and Pin-Fins

Journals

Conference Proceedings

eBooks

Resources

Opportunities

Journals

Conference Proceedings

eBooks

Resources

Opportunities

This Feature Is Available To Subscribers Only