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Journal Articles

Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles

Shane Haydt, Stephen Lynch
Journal: Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach. May 2021, 143(5): 051012.
Paper No: TURBO-19-1318
DOI: https://doi.org/10.1115/1.4046964
Published Online: April 15, 2021
View Article titled, Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles
Click here to open pdf in another window PDF for Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles
Topics: Coolants, Film cooling, Heat flux, Heat transfer coefficients, Temperature, Vortices, Flow (Dynamics), Heat transfer, Flat plates
Proceedings Papers

A Steady Transonic Linear Cascade for True Scale Cooling Measurements

Jeremy Zuccarello, David Saltzman, Stephen Lynch, Shane Haydt, Christopher Whitfield
Proc. ASME. GT2020, Volume 7C: Heat Transfer, V07CT13A001, September 21–25, 2020
Paper No: GT2020-14269
DOI: https://doi.org/10.1115/GT2020-14269
View Paper titled, A Steady Transonic Linear Cascade for True Scale Cooling Measurements
Click here to open pdf in another window PDF for A Steady Transonic Linear Cascade for True Scale Cooling Measurements
Topics: Cascades (Fluid dynamics), Cooling, Airfoils, Lasers, Blades, Flow (Dynamics), Glass, Reynolds number, Boundary layers, Chords (Trusses)
Proceedings Papers

Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles

Shane Haydt, Stephen Lynch
Proc. ASME. GT2019, Volume 5B: Heat Transfer, V05BT19A026, June 17–21, 2019
Paper No: GT2019-91870
DOI: https://doi.org/10.1115/GT2019-91870
View Paper titled, Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles
Click here to open pdf in another window PDF for Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles
Topics: Film cooling, Heat transfer coefficients, Coolants, Heat flux, Temperature, Convection, Gas turbines, Heat transfer, Metals, Thermography
Journal Articles

Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles

Shane Haydt, Stephen Lynch
Journal: Journal of Turbomachinery
Article Type: Research-Article
J. Turbomach. April 2019, 141(4): 041005.
Paper No: TURBO-18-1238
DOI: https://doi.org/10.1115/1.4041603
Published Online: January 21, 2019
View Article titled, Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles
Click here to open pdf in another window PDF for Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles
Topics: Computational fluid dynamics, Coolants, Film cooling, Jets, Flow (Dynamics), Cooling
Proceedings Papers

Flowfield of a Shaped Film Cooling Hole Over a Range of Compound Angles

Shane Haydt, Stephen Lynch
Proc. ASME. GT2018, Volume 5C: Heat Transfer, V05CT19A012, June 11–15, 2018
Paper No: GT2018-75728
DOI: https://doi.org/10.1115/GT2018-75728
View Paper titled, Flowfield of a Shaped Film Cooling Hole Over a Range of Compound Angles
Click here to open pdf in another window PDF for Flowfield of a Shaped Film Cooling Hole Over a Range of Compound Angles
Topics: Film cooling, Vortices, Coolants, Cooling, Density, Gas turbines, Heat transfer coefficients, Metals, Particulate matter, Temperature
Proceedings Papers

Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles

Shane Haydt, Stephen Lynch
Proc. ASME. GT2018, Volume 5C: Heat Transfer, V05CT19A011, June 11–15, 2018
Paper No: GT2018-75726
DOI: https://doi.org/10.1115/GT2018-75726
View Paper titled, Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles
Click here to open pdf in another window PDF for Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles
Topics: Cooling, Film cooling, Computational fluid dynamics, Convection, Coolants, Temperature, Density, Gas turbines, Metals, Reynolds-averaged Navier–Stokes equations
Journal Articles

The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes With Constant Expansion Angles

Shane Haydt, Stephen Lynch, Scott Lewis
Journal: Journal of Turbomachinery
Article Type: Research-Article
J. Turbomach. May 2018, 140(5): 051002.
Paper No: TURBO-17-1183
DOI: https://doi.org/10.1115/1.4038871
Published Online: February 27, 2018
View Article titled, The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes With Constant Expansion Angles
Click here to open pdf in another window PDF for The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes With Constant Expansion Angles
Topics: Coolants, Diffusers, Film cooling, Flow (Dynamics), Computational fluid dynamics, Particulate matter, Diffusion (Physics)
Proceedings Papers

The Effect of Area Ratio Change via Increased Hole Length for Shaped Film Cooling Holes With Constant Expansion Angles

Shane Haydt, Stephen Lynch, Scott Lewis
Proc. ASME. GT2017, Volume 5C: Heat Transfer, V05CT19A009, June 26–30, 2017
Paper No: GT2017-63692
DOI: https://doi.org/10.1115/GT2017-63692
View Paper titled, The Effect of Area Ratio Change via Increased Hole Length for Shaped Film Cooling Holes With Constant Expansion Angles
Click here to open pdf in another window PDF for The Effect of Area Ratio Change via Increased Hole Length for Shaped Film Cooling Holes With Constant Expansion Angles
Topics: Film cooling, Diffusers, Coolants, Cooling, Diffusion (Physics), Momentum, Shapes, Durability, Engineering simulation, Flow (Dynamics)
Journal Articles

The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness

Shane Haydt, Stephen Lynch, Scott Lewis
Journal: Journal of Turbomachinery
Article Type: Research-Article
J. Turbomach. September 2017, 139(9): 091012.
Paper No: TURBO-16-1299
DOI: https://doi.org/10.1115/1.4036199
Published Online: May 2, 2017
View Article titled, The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness
Click here to open pdf in another window PDF for The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness
Topics: Coolants, Diffusers, Film cooling, Temperature, Computational fluid dynamics, Momentum, Cooling
Proceedings Papers

The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness

Shane Haydt, Stephen Lynch, Scott Lewis
Proc. ASME. GT2016, Volume 5C: Heat Transfer, V05CT19A002, June 13–17, 2016
Paper No: GT2016-56135
DOI: https://doi.org/10.1115/GT2016-56135
View Paper titled, The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness
Click here to open pdf in another window PDF for The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness
Topics: Diffusers, Film cooling, Coolants, Cooling, Density, Electrical discharge machining, Gas turbines, Manufacturing, Momentum, Reynolds-averaged Navier–Stokes equations