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Proceedings Papers

Determination of Cooling Parameters for a High Speed, True Scale, Metallic Turbine Vane Ring

M. D. Polanka, R. J. Anthony, David G. Bogard, Mark F. Reeder

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 233-245, June 9–13, 2008

Paper No: GT2008-50281

DOI: https://doi.org/10.1115/GT2008-50281

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Topics: Cooling, Turbines, Temperature, Airfoils, Film cooling, Flow (Dynamics), Coolants, Engines, Heat transfer, Air Force

Proceedings Papers

An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes

M. D. Barringer, M. D. Polanka, K. A. Thole

Proc. ASME. GT2007, Volume 4: Turbo Expo 2007, Parts A and B, 1323-1334, May 14–17, 2007

Paper No: GT2007-27156

DOI: https://doi.org/10.1115/GT2007-27156

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Topics: Combustion chambers, Heat transfer, High pressure (Physics), Shapes, Turbines, Temperature, Pressure, Air Force, Aircraft propulsion, Airfoils

Proceedings Papers

Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes

M. D. Barringer, M. D. Polanka, J. P. Clark, P. J. Koch, K. A. Thole

Proc. ASME. GT2007, Volume 4: Turbo Expo 2007, Parts A and B, 1335-1346, May 14–17, 2007

Paper No: GT2007-27157

DOI: https://doi.org/10.1115/GT2007-27157

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Topics: Combustion chambers, High pressure (Physics), Turbines, Flow (Dynamics), Pressure, Gas turbines, Temperature, Air Force, Airfoils, Enthalpy

Proceedings Papers

Turbine Tip and Shroud Heat Transfer and Loading: Part B — Comparisons Between Prediction and Experiment Including Unsteady Effects

M. D. Polanka, J. P. Clark, A. L. White, M. Meininger, T. J. Praisner

Proc. ASME. GT2003, Volume 5: Turbo Expo 2003, Parts A and B, 691-702, June 16–19, 2003

Paper No: GT2003-38916

DOI: https://doi.org/10.1115/GT2003-38916

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Topics: Heat transfer, Turbines, Blades, Flow (Dynamics), Physics, Air Force, Airfoils, Annulus, Collaboration, Heat

Journal Articles

An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes

M. D. Barringer, K. A. Thole, M. D. Polanka

J. Turbomach. April 2009, 131(2): 021009.

DOI: https://doi.org/10.1115/1.2950072

Published Online: January 23, 2009

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Topics: Flow (Dynamics), Gages, Heat transfer, Pressure, Shapes, Temperature, Turbines, Combustion chambers, High pressure (Physics), Convection

Journal Articles

Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes

M. D. Barringer, K. A. Thole, M. D. Polanka, J. P. Clark, P. J. Koch

J. Turbomach. April 2009, 131(2): 021010.

DOI: https://doi.org/10.1115/1.2950076

Published Online: January 23, 2009

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Topics: Flow (Dynamics), Pressure, Turbines, Temperature, High pressure (Physics), Combustion chambers, Turbulence, Shapes

Journal Articles

Effects of Combustor Exit Profiles on Vane Aerodynamic Loading and Heat Transfer in a High Pressure Turbine

M. D. Barringer, K. A. Thole, M. D. Polanka

J. Turbomach. April 2009, 131(2): 021008.

DOI: https://doi.org/10.1115/1.2950051

Published Online: January 23, 2009

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Topics: Combustion chambers, Flow (Dynamics), Heat transfer, High pressure (Physics), Pressure, Temperature, Turbines, Temperature profiles

Proceedings Papers

Developing a Combustor Simulator for Investigating High Pressure Turbine Aerodynamics and Heat Transfer

M. D. Barringer, K. A. Thole, M. D. Polanka

Proc. ASME. GT2004, Volume 3: Turbo Expo 2004, 565-575, June 14–17, 2004

Paper No: GT2004-53613

DOI: https://doi.org/10.1115/GT2004-53613

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Topics: Aerodynamics, Combustion chambers, Heat transfer, High pressure (Physics), Turbines, Pressure, Temperature, Design, Turbulence, Film cooling

Proceedings Papers

Numerical Modeling of Flow and Thermal Patterns Within a Combustor Simulator

V. R. Kunze, M. Wolff, M. D. Barringer, K. A. Thole, M. D. Polanka

Proc. ASME. GT2005, Volume 6: Turbo Expo 2005, Parts A and B, 519-528, June 6–9, 2005

Paper No: GT2005-68284

DOI: https://doi.org/10.1115/GT2005-68284

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Topics: Combustion chambers, Computer simulation, Flow (Dynamics), Turbines, Computational fluid dynamics, Heat transfer, Shapes, Temperature, Air Force, Airfoils

Proceedings Papers

Numerical Insight Into Flow and Thermal Patterns Within an Inlet Profile Generator Comparing to Experimental Results

V. R. Kunze, M. Wolff, M. D. Barringer, K. A. Thole, M. D. Polanka

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 271-283, May 8–11, 2006

Paper No: GT2006-90276

DOI: https://doi.org/10.1115/GT2006-90276

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Topics: Flow (Dynamics), Generators, Combustion chambers, Turbines, Computational fluid dynamics, Design, Air Force, Boundary layer turbulence, Gas turbines, High pressure (Physics)

Proceedings Papers

Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer

M. D. Barringer, K. A. Thole, M. D. Polanka

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 285-295, May 8–11, 2006

Paper No: GT2006-90277

DOI: https://doi.org/10.1115/GT2006-90277

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Topics: Aerodynamics, Combustion chambers, Heat transfer, High pressure (Physics), Turbines, Pressure, Temperature profiles, Air Force, Aircraft engines, Generators

Proceedings Papers

Experimental Evaluation of an Inlet Profile Generator for High Pressure Turbine Tests

M. D. Barringer, K. A. Thole, M. D. Polanka

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 447-458, May 8–11, 2006

Paper No: GT2006-90401

DOI: https://doi.org/10.1115/GT2006-90401

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Topics: Generators, High pressure (Physics), Turbines, Combustion chambers, Flow (Dynamics), Heat transfer, Pressure, Temperature, Turbulence, Aerodynamics

Journal Articles

Experimental Evaluation of an Inlet Profile Generator for High-Pressure Turbine Tests

M. D. Barringer, K. A. Thole, M. D. Polanka

J. Turbomach. April 2007, 129(2): 382–393.

DOI: https://doi.org/10.1115/1.2436897

Published Online: July 31, 2006

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Topics: Combustion chambers, Flow (Dynamics), Generators, Pressure, Temperature, Temperature profiles, Turbines, Turbulence, Film cooling, Heat transfer

Journal citation

NARROW

Determination of Cooling Parameters for a High Speed, True Scale, Metallic Turbine Vane Ring

An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes

Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes

Turbine Tip and Shroud Heat Transfer and Loading: Part B — Comparisons Between Prediction and Experiment Including Unsteady Effects

An Experimental Study of Combustor Exit Profile Shapes on Endwall Heat Transfer in High Pressure Turbine Vanes

Migration of Combustor Exit Profiles Through High Pressure Turbine Vanes

Effects of Combustor Exit Profiles on Vane Aerodynamic Loading and Heat Transfer in a High Pressure Turbine

Developing a Combustor Simulator for Investigating High Pressure Turbine Aerodynamics and Heat Transfer

Numerical Modeling of Flow and Thermal Patterns Within a Combustor Simulator

Numerical Insight Into Flow and Thermal Patterns Within an Inlet Profile Generator Comparing to Experimental Results

Effects of Combustor Exit Profiles on High Pressure Turbine Vane Aerodynamics and Heat Transfer

Experimental Evaluation of an Inlet Profile Generator for High Pressure Turbine Tests

Experimental Evaluation of an Inlet Profile Generator for High-Pressure Turbine Tests

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