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Proceedings Papers

Indirect Turbulence Measurement in Gas Turbine Stages Using Heat Flux Probe

Luzeng J. Zhang, Boris Glezer

Proc. ASME. GT1995, Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, V004T09A041, June 5–8, 1995

Paper No: 95-GT-153

DOI: https://doi.org/10.1115/95-GT-153

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Topics: Gas turbines, Heat flux, Probes, Turbulence, Combustion chambers, Blades, Wakes, Airfoils, Cascades (Fluid dynamics), Engine design

Proceedings Papers

Color Response Modification of Encapsulated Liquid Crystals Used in Rotating Disk Heat Transfer Studies

Cengiz Camci, Boris Glezer

Proc. ASME. GT1995, Volume 1: Turbomachinery, V001T01A104, June 5–8, 1995

Paper No: 95-GT-439

DOI: https://doi.org/10.1115/95-GT-439

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Topics: Heat transfer, Liquid crystals, Rotating disks, Temperature, Coatings, Aluminum, Calibration, Collapse, Disks, Energy budget (Physics)

Proceedings Papers

Turbine Airfoil External Heat Transfer Measurement in a Hot-Cascade

Luzeng J. Zhang, Boris Glezer

Proc. ASME. GT1997, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T09A063, June 2–5, 1997

Paper No: 97-GT-327

DOI: https://doi.org/10.1115/97-GT-327

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Topics: Airfoils, Cascades (Fluid dynamics), Heat transfer, Turbines, Heat transfer coefficients, Temperature, Calibration, Coolants, Turbulence, Boundary layers

Proceedings Papers

Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1 — Effect of Cut-Back Length, Spanwise Rib Spacing, Free Stream Reynolds Number and Chordwise Rib Length on Discharge Coefficients

Oğuz Uzol, Cengiz Camcı, Boris Glezer

Proc. ASME. GT2000, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A064, May 8–11, 2000

Paper No: 2000-GT-0258

DOI: https://doi.org/10.1115/2000-GT-0258

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Topics: Coolants, Discharge coefficient, Reynolds number, Turbine blades, Cooling systems, Flow (Dynamics), Blades, Fluid mechanics, Fluids, Pressure

Proceedings Papers

Integration of Multi-Disciplinary Factors Into Turbine Cooling Design

Boris Glezer

Proc. ASME. GT2001, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A055, June 4–7, 2001

Paper No: 2001-GT-0179

DOI: https://doi.org/10.1115/2001-GT-0179

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Topics: Cooling, Design, Turbines, Blades, Engineering disciplines, Combustion chambers, Disks, Engines, Gas turbines, Nozzles

Proceedings Papers

Mainstream Aerodynamic Effects due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I — Aerodynamic Measurements in the Stationary Frame

Christopher McLean, Cengiz Camci, Boris Glezer

Proc. ASME. GT2001, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A006, June 4–7, 2001

Paper No: 2001-GT-0119

DOI: https://doi.org/10.1115/2001-GT-0119

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Topics: Coolants, High pressure (Physics), Turbines, Cooling, Rotors, Axial flow, Boundary layers, Cavities, Flow (Dynamics), Impingement cooling

Proceedings Papers

Mainstream Aerodynamic Effects due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II — Aerodynamic Measurements in the Rotational Frame

Christopher McLean, Cengiz Camci, Boris Glezer

Proc. ASME. GT2001, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A007, June 4–7, 2001

Paper No: 2001-GT-0120

DOI: https://doi.org/10.1115/2001-GT-0120

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Topics: Coolants, High pressure (Physics), Turbines, Cooling, Flow (Dynamics), Rotors, Nozzle guide vanes, Axial flow, Boundary layers, Impingement cooling

Proceedings Papers

Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45° Angled Rib Turbulators

Gm. S. Azad, Mohammad J. Uddin, Je-Chin Han, Hee-Koo Moon, Boris Glezer

Proc. ASME. GT2001, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A061, June 4–7, 2001

Paper No: 2001-GT-0186

DOI: https://doi.org/10.1115/2001-GT-0186

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Topics: Heat transfer, Rotation, Coolants, Density, Flow (Dynamics), Heat transfer coefficients, Reynolds number

Proceedings Papers

Numerical and Experimental Study of Ventilation for Gas Turbine Package Enclosure

Daniel Vahidi, Hamid Bagheri, Boris Glezer

Proc. ASME. GT2006, Volume 5: Marine; Microturbines and Small Turbomachinery; Oil and Gas Applications; Structures and Dynamics, Parts A and B, 607-616, May 8–11, 2006

Paper No: GT2006-90960

DOI: https://doi.org/10.1115/GT2006-90960

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Topics: Gas turbines, Ventilation, Engines, Carbon dioxide, Computational fluid dynamics, Design, Boundary-value problems, Flow (Dynamics), Flow visualization, Imaging

Journal Articles

Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators

Gm S. Azad, Mohammad J. Uddin, Je-Chin Han, Hee-Koo Moon, Boris Glezer

J. Turbomach. April 2002, 124(2): 251–259.

DOI: https://doi.org/10.1115/1.1450569

Published Online: April 9, 2002

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Topics: Flow (Dynamics), Heat transfer, Heat transfer coefficients, Rotation, Reynolds number, Coolants, Gas turbines

Journal Articles

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame

Christopher McLean, Cengiz Camci, Professor of Aerospace Engineering, Boris Glezer

J. Turbomach. October 2001, 123(4): 697–703.

DOI: https://doi.org/10.1115/1.1397303

Published Online: February 1, 2001

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Topics: Coolants, Cooling, Flow (Dynamics), High pressure (Physics), Pressure, Rotors, Turbines, Wakes, Impingement cooling, Probes

Journal Articles

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame

Christopher McLean, Cengiz Camci, Professor of Aerospace Engineering, Boris Glezer

J. Turbomach. October 2001, 123(4): 687–696.

DOI: https://doi.org/10.1115/1.1401026

Published Online: February 1, 2001

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Topics: Coolants, Cooling, Flow (Dynamics), Pressure, Rotors, Turbines, Uncertainty, Impingement cooling, High pressure (Physics)

Journal Articles

Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1—Effect of Cut-Back Length, Spanwise Rib Spacing, Free-Stream Reynolds Number, and Chordwise Rib Length on Discharge Coefficients

Oguz Uzol, Cengiz Camci, Boris Glezer

J. Turbomach. April 2001, 123(2): 238–248.

DOI: https://doi.org/10.1115/1.1348017

Published Online: February 1, 2000

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Topics: Coolants, Discharge coefficient, Flow (Dynamics), Pressure, Reynolds number

Journal citation

NARROW

Indirect Turbulence Measurement in Gas Turbine Stages Using Heat Flux Probe

Color Response Modification of Encapsulated Liquid Crystals Used in Rotating Disk Heat Transfer Studies

Turbine Airfoil External Heat Transfer Measurement in a Hot-Cascade

Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1 — Effect of Cut-Back Length, Spanwise Rib Spacing, Free Stream Reynolds Number and Chordwise Rib Length on Discharge Coefficients

Integration of Multi-Disciplinary Factors Into Turbine Cooling Design

Mainstream Aerodynamic Effects due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I — Aerodynamic Measurements in the Stationary Frame

Mainstream Aerodynamic Effects due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II — Aerodynamic Measurements in the Rotational Frame

Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45° Angled Rib Turbulators

Numerical and Experimental Study of Ventilation for Gas Turbine Package Enclosure

Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame

Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1—Effect of Cut-Back Length, Spanwise Rib Spacing, Free-Stream Reynolds Number, and Chordwise Rib Length on Discharge Coefficients

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