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Harika S. Kahveci
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Journal Articles

Investigation of a Rotor Blade With Tip Cooling Subject to a Nonuniform Temperature Profile

Harika S. Kahveci
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2021, 143(7): 071002.
Paper No: TURBO-20-1255
https://doi.org/10.1115/1.4050332
Published Online: April 8, 2021
View Article titled, Investigation of a Rotor Blade With Tip Cooling Subject to a Nonuniform Temperature Profile
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Topics: Blades, Cooling, Temperature profiles, Pressure, Heat transfer, Flow (Dynamics), Coolants, Temperature
Proceedings Papers

Investigation of a Rotor Blade With Tip Cooling Subject to a Nonuniform Temperature Profile

Harika S. Kahveci
Proc. ASME. GT2020, Volume 7B: Heat Transfer, V07BT12A052, September 21–25, 2020
Publisher: American Society of Mechanical Engineers
Paper No: GT2020-15529
https://doi.org/10.1115/GT2020-15529
View Paper titled, Investigation of a Rotor Blade With Tip Cooling Subject to a Nonuniform Temperature Profile
Open the PDF for Investigation of a Rotor Blade With Tip Cooling Subject to a Nonuniform Temperature Profile in another window
Topics: Blades, Cooling, Rotors, Temperature profiles, Pressure, Coolants, Design, Flow (Dynamics), Heat transfer, Turbine blades
Journal Articles

Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer

Sergen Sakaoglu, Harika S. Kahveci
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. February 2020, 142(2): 021008.
Paper No: TURBO-19-1274
https://doi.org/10.1115/1.4045466
Published Online: January 24, 2020
View Article titled, Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer
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Topics: Blades, Clearances (Engineering), Cooling, Flow (Dynamics), Heat transfer, Leakage flows, Pressure, Turbine blades, Coolants, Aerodynamics
Proceedings Papers

Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer

Sergen Sakaoglu, Harika S. Kahveci
Proc. ASME. GT2019, Volume 5A: Heat Transfer, V05AT12A001, June 17–21, 2019
Publisher: American Society of Mechanical Engineers
Paper No: GT2019-90130
https://doi.org/10.1115/GT2019-90130
View Paper titled, Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer
Open the PDF for Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer in another window
Topics: Cooling, Heat transfer, Leakage flows, Turbine blades, Pressure, Blades, Aerodynamics, Coolants, Clearances (Engineering), Design
Journal Articles

Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine

Harika S. Kahveci, Kevin R. Kirtley
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. June 2014, 136(6): 061020.
Paper No: TURBO-13-1208
https://doi.org/10.1115/1.4025764
Published Online: December 4, 2013
View Article titled, Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine
Open the PDF for Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine in another window
Topics: Blades, Computational fluid dynamics, Cooling, Gages, Heat transfer, Surface roughness, Turbines, Uncertainty, Temperature profiles, Flow (Dynamics)
Proceedings Papers

Comparison of Temperature Profile and Heat Transfer Predictions With Statistically-Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine

Harika S. Kahveci, Kevin R. Kirtley
Proc. ASME. GT2013, Volume 3C: Heat Transfer, V03CT14A001, June 3–7, 2013
Publisher: American Society of Mechanical Engineers
Paper No: GT2013-94242
https://doi.org/10.1115/GT2013-94242
View Paper titled, Comparison of Temperature Profile and Heat Transfer Predictions With Statistically-Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine
Open the PDF for Comparison of Temperature Profile and Heat Transfer Predictions With Statistically-Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine in another window
Topics: Heat transfer, High pressure (Physics), Temperature profiles, Turbines, Uncertainty, Blades, Computational fluid dynamics, Cooling, Gages, Surface roughness
Journal Articles

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall

Harika S. Kahveci, Charles W. Haldeman, Randall M. Mathison, Michael G. Dunn
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. March 2013, 135(2): 021028.
Paper No: TURBO-11-1145
https://doi.org/10.1115/1.4006776
Published Online: November 8, 2012
View Article titled, Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall
Open the PDF for Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall in another window
Topics: Cooling, Flow (Dynamics), Heat transfer, Airfoils, Coolants
Journal Articles

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Harika S. Kahveci, Charles W. Haldeman, Randall M. Mathison, Michael G. Dunn
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. March 2013, 135(2): 021027.
Paper No: TURBO-11-1144
https://doi.org/10.1115/1.4006775
Published Online: November 1, 2012
View Article titled, Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects
Open the PDF for Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects in another window
Topics: Cooling, Flow (Dynamics), Heat flux, Heat transfer, Temperature, Temperature profiles, Airfoils, Pressure, Turbines, Coolants
Proceedings Papers

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part II—Effect of Cooling Variation on the Vane Airfoil and Inner Endwall

Harika S. Kahveci, Charles W. Haldeman, Randall M. Mathison, Michael G. Dunn
Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 1735-1744, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-46573
https://doi.org/10.1115/GT2011-46573
View Paper titled, Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part II—Effect of Cooling Variation on the Vane Airfoil and Inner Endwall
Open the PDF for Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part II—Effect of Cooling Variation on the Vane Airfoil and Inner Endwall in another window
Topics: Airfoils, Cooling, Heat transfer, High pressure (Physics), Turbine components, Coolants, Flow (Dynamics), Circuits, Pressure, Temperature profiles
Proceedings Papers

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part I—Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Harika S. Kahveci, Charles W. Haldeman, Randall M. Mathison, Michael G. Dunn
Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 1719-1733, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-46570
https://doi.org/10.1115/GT2011-46570
View Paper titled, Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part I—Experimental Configuration and Data Review With Inlet Temperature Profile Effects
Open the PDF for Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine: Part I—Experimental Configuration and Data Review With Inlet Temperature Profile Effects in another window
Topics: Heat transfer, High pressure (Physics), Temperature profiles, Turbine components, Cooling, Airfoils, Circuits, Coolants, Flow (Dynamics), Pressure
Journal Articles

Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design

Philip L. Andrew, Harika S. Kahveci
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2009, 131(3): 031013.
https://doi.org/10.1115/1.2988165
Published Online: April 10, 2009
View Article titled, Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design
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Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Design, Mach number, Pressure, Flow (Dynamics), Turbines, High pressure (Physics)
Proceedings Papers

Validation of MISES 2-D Boundary Layer Code for High Pressure Turbine Aerodynamic Design

Philip L. Andrew, Harika S. Kahveci
Proc. ASME. GT2007, Volume 6: Turbo Expo 2007, Parts A and B, 879-893, May 14–17, 2007
Publisher: American Society of Mechanical Engineers
Paper No: GT2007-28123
https://doi.org/10.1115/GT2007-28123
View Paper titled, Validation of MISES 2-D Boundary Layer Code for High Pressure Turbine Aerodynamic Design
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Topics: Boundary layers, Cascades (Fluid dynamics), Design, High pressure (Physics), Turbines