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Paul I. King
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Proceedings Papers

Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor

Donald W. Thompson, Paul I. King, Douglas C. Rabe
Proc. ASME. GT1997, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A002, June 2–5, 1997
Publisher: American Society of Mechanical Engineers
Paper No: 97-GT-007
https://doi.org/10.1115/97-GT-007
View Paper titled, Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor
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Topics: Axial flow, Compressors, Rotors, Clearances (Engineering), Flow (Dynamics), Design, Engineers, Inlet guide vanes, Pressure
Proceedings Papers

Experimental and Computational Investigation of Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor

Donald W. Thompson, Paul I. King, Chunill Hah, Douglas C. Rabe
Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A026, June 2–5, 1998
Publisher: American Society of Mechanical Engineers
Paper No: 98-GT-090
https://doi.org/10.1115/98-GT-090
View Paper titled, Experimental and Computational Investigation of Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor
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Topics: Axial flow, Compressors, Rotors, Clearances (Engineering), Flow (Dynamics), Geometry, Computational fluid dynamics, Design, Engineers, Inlet guide vanes
Journal Articles

Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part I: Airfoil Design

M. Eric Lyall, Paul I. King, John P. Clark, Rolf Sondergaard
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. August 2014, 136(8): 081005.
Paper No: TURBO-13-1195
https://doi.org/10.1115/1.4025951
Published Online: January 31, 2014
View Article titled, Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part I: Airfoil Design
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Topics: Airfoils, Design, Pressure
Proceedings Papers

Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring: Part I — Airfoil Design

M. Eric Lyall, Paul I. King, John P. Clark, Rolf Sondergaard
Proc. ASME. GT2013, Volume 6A: Turbomachinery, V06AT36A023, June 3–7, 2013
Publisher: American Society of Mechanical Engineers
Paper No: GT2013-95000
https://doi.org/10.1115/GT2013-95000
View Paper titled, Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring: Part I — Airfoil Design
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Topics: Airfoils, Design, Pressure, Turbines, Cascades (Fluid dynamics)
Proceedings Papers

Endwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade

M. Eric Lyall, Paul I. King, Rolf Sondergaard
Proc. ASME. GT2012, Volume 8: Turbomachinery, Parts A, B, and C, 1205-1216, June 11–15, 2012
Publisher: American Society of Mechanical Engineers
Paper No: GT2012-68709
https://doi.org/10.1115/GT2012-68709
View Paper titled, Endwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade
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Topics: Cascades (Fluid dynamics), Pressure, Turbines, Flow (Dynamics), Turbulence, Separation (Technology), Shear (Mechanics), Suction, Vortices, Boundary layers
Journal Articles

Endwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade

M. Eric Lyall, Paul I. King, Rolf Sondergaard
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. September 2013, 135(5): 051006.
Paper No: TURBO-12-1033
https://doi.org/10.1115/1.4007801
Published Online: June 26, 2013
View Article titled, Endwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade
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Topics: Cascades (Fluid dynamics), Flow (Dynamics), Pressure, Turbulence, Suction, Boundary layers
Proceedings Papers

Performance of a Turbine Driven by a Pulsed Detonation Combustor

Kurt P. Rouser, Paul I. King, Frederick R. Schauer, Rolf Sondergaard, John L. Hoke
Proc. ASME. IMECE2011, Volume 1: Advances in Aerospace Technology; Energy Water Nexus; Globalization of Engineering; Posters, 51-62, November 11–17, 2011
Publisher: American Society of Mechanical Engineers
Paper No: IMECE2011-64385
https://doi.org/10.1115/IMECE2011-64385
View Paper titled, Performance of a Turbine Driven by a Pulsed Detonation Combustor
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Topics: Combustion chambers, Explosions, Turbines, Cycles, Pressure, Combustion, Enthalpy, Flow (Dynamics), Compressors, Engines
Journal Articles

An Investigation of Reynolds Lapse Rate for Highly Loaded Low Pressure Turbine Airfoils With Forward and Aft Loading

M. Eric Lyall, Paul I. King, Rolf Sondergaard, John P. Clark, Mark W. McQuilling
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. September 2012, 134(5): 051035.
https://doi.org/10.1115/1.4004826
Published Online: May 24, 2012
View Article titled, An Investigation of Reynolds Lapse Rate for Highly Loaded Low Pressure Turbine Airfoils With Forward and Aft Loading
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Topics: Airfoils, Pressure, Reynolds number, Suction, Turbulence, Flow (Dynamics), Cascades (Fluid dynamics), Boundary layers, Turbines, Reynolds-averaged Navier–Stokes equations
Journal Articles

Influence of Film Cooling Unsteadiness on Turbine Blade Leading Edge Heat Flux

James L. Rutledge, Paul I. King, Richard B. Rivir
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Gas Turbines: Heat Transfer
J. Eng. Gas Turbines Power. July 2012, 134(7): 071901.
https://doi.org/10.1115/1.4005978
Published Online: May 23, 2012
View Article titled, Influence of Film Cooling Unsteadiness on Turbine Blade Leading Edge Heat Flux
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Topics: Film cooling, Heat flux, Coolants, Waves, Turbine blades, Cooling, Flow (Dynamics)
Proceedings Papers

Performance Evaluation of an Unsteady Turbine Driven by a Pulsed Detonation Combustor

Kurt P. Rouser, Paul I. King, Frederick R. Schauer, Rolf Sondergaard, John L. Hoke
Proc. ASME. GT2011, Volume 7: Turbomachinery, Parts A, B, and C, 1503-1516, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-45396
https://doi.org/10.1115/GT2011-45396
View Paper titled, Performance Evaluation of an Unsteady Turbine Driven by a Pulsed Detonation Combustor
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Topics: Combustion chambers, Explosions, Performance evaluation, Turbines, Pressure, Flow (Dynamics), Rotors, Temperature, Torque, Brayton cycle
Proceedings Papers

An Investigation of Reynolds Lapse Rate for Highly Loaded Low Pressure Turbine Airfoils With Forward and Aft Loading

M. Eric Lyall, Paul I. King, Rolf Sondergaard, John P. Clark, Mark W. McQuilling
Proc. ASME. GT2011, Volume 7: Turbomachinery, Parts A, B, and C, 865-876, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-46328
https://doi.org/10.1115/GT2011-46328
View Paper titled, An Investigation of Reynolds Lapse Rate for Highly Loaded Low Pressure Turbine Airfoils With Forward and Aft Loading
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Topics: Airfoils, Pressure, Turbines, Turbulence, Reynolds number, Eddies (Fluid dynamics), Sensors, Viscosity, Anisotropy, Chords (Trusses)
Proceedings Papers

Flow Visualization Study of Passive Flow Control Features on a Film-Cooled Turbine Blade Leading Edge

Daniel R. Carroll, Paul I. King, James L. Rutledge
Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 1739-1750, June 14–18, 2010
Publisher: American Society of Mechanical Engineers
Paper No: GT2010-23179
https://doi.org/10.1115/GT2010-23179
View Paper titled, Flow Visualization Study of Passive Flow Control Features on a Film-Cooled Turbine Blade Leading Edge
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Topics: Flow control, Flow visualization, Turbine blades, Coolants, Flow (Dynamics), Geometry, Water
Journal Articles

Time Averaged Net Heat Flux Reduction for Unsteady Film Cooling

James L. Rutledge, Paul I. King, Richard Rivir
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. December 2010, 132(12): 121901.
https://doi.org/10.1115/1.4001810
Published Online: August 24, 2010
View Article titled, Time Averaged Net Heat Flux Reduction for Unsteady Film Cooling
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Topics: Film cooling, Flow (Dynamics), Fluctuations (Physics), Heat flux, Temperature, Coolants, Gas turbines, Heat conduction
Proceedings Papers

CFD Predictions of Pulsed Film Cooling Heat Flux on a Turbine Blade Leading Edge

James L. Rutledge, Paul I. King, Richard Rivir
Proc. ASME. IMECE2008, Volume 10: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A, B, and C, 1139-1149, October 31–November 6, 2008
Publisher: American Society of Mechanical Engineers
Paper No: IMECE2008-67276
https://doi.org/10.1115/IMECE2008-67276
View Paper titled, CFD Predictions of Pulsed Film Cooling Heat Flux on a Turbine Blade Leading Edge
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Topics: Computational fluid dynamics, Film cooling, Heat flux, Turbine blades, Coolants, Flow (Dynamics), Blades, Cycles, Engineering simulation, Flow control