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Journal Articles

Heat Transfer and Pressure Drop Correlations for Square Channels With 45 Deg Ribs at High Reynolds Numbers

Akhilesh P. Rallabandi, Huitao Yang, Je-Chin Han

Publisher: ASME

J. Heat Mass Transfer. July 2009, 131(7): 071703.

https://doi.org/10.1115/1.3090818

Published Online: May 14, 2009

View Article titled, Heat Transfer and Pressure Drop Correlations for Square Channels With 45 Deg Ribs at High Reynolds Numbers

Topics: Friction, Heat transfer, Reynolds number, Heat transfer coefficients, Pressure drop, Flow (Dynamics)

Proceedings Papers

Flow and Heat Transfer Predictions for a Flat-Tip Turbine Blade

Huitao Yang, Sumanta Acharya, Srinath V. Ekkad, Chander Prakash, Ron Bunker

Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 271-283, June 3–6, 2002

Publisher: American Society of Mechanical Engineers

Paper No: GT2002-30190

https://doi.org/10.1115/GT2002-30190

View Paper titled, Flow and Heat Transfer Predictions for a Flat-Tip Turbine Blade

Topics: Flow (Dynamics), Heat transfer, Turbine blades, Blades, Pressure, Turbulence, Stress, Leakage flows, Rotors, Turbines

Proceedings Papers

Numerical Simulation of Film Cooling on the Tip of a Gas Turbine Blade

Sumanta Acharya, Huitao Yang, Srinath V. Ekkad, Chander Prakash, Ron Bunker

Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 1051-1062, June 3–6, 2002

Publisher: American Society of Mechanical Engineers

Paper No: GT2002-30553

https://doi.org/10.1115/GT2002-30553

View Paper titled, Numerical Simulation of Film Cooling on the Tip of a Gas Turbine Blade

Topics: Blades, Computer simulation, Film cooling, Gas turbines, Coolants, Flow (Dynamics), Trajectories (Physics), Cavities, Heat transfer, Heat transfer coefficients

Proceedings Papers

Numerical Simulation of Flow and Heat Transfer Past a Turbine Blade With a Squealer-Tip

Huitao Yang, Sumanta Acharya, Srinath V. Ekkad, Chander Prakash, Ron Bunker

Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 295-307, June 3–6, 2002

Publisher: American Society of Mechanical Engineers

Paper No: GT2002-30193

https://doi.org/10.1115/GT2002-30193

View Paper titled, Numerical Simulation of Flow and Heat Transfer Past a Turbine Blade With a Squealer-Tip

Topics: Computer simulation, Flow (Dynamics), Heat transfer, Turbine blades, Blades, Leakage flows, Stress, Turbulence, Heat transfer coefficients, Pressure

Proceedings Papers

Numerical Study of Flow and Heat Transfer on a Blade Tip With Different Leakage Reduction Strategies

Sumanta Acharya, Huitao Yang, Chander Prakash, Ron Bunker

Proc. ASME. GT2003, Volume 5: Turbo Expo 2003, Parts A and B, 471-480, June 16–19, 2003

Publisher: American Society of Mechanical Engineers

Paper No: GT2003-38617

https://doi.org/10.1115/GT2003-38617

View Paper titled, Numerical Study of Flow and Heat Transfer on a Blade Tip With Different Leakage Reduction Strategies

Topics: Blades, Flow (Dynamics), Heat transfer, Leakage, Pressure, Leakage flows, Suction, Heat transfer coefficients, Clearances (Engineering), Rotors

Proceedings Papers

Numerical Prediction of Film Cooling and Heat Transfer With Different Film-Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade

Huitao Yang, Hamn-Ching Chen, Je-Chin Han

Proc. ASME. GT2004, Volume 3: Turbo Expo 2004, 177-187, June 14–17, 2004

Publisher: American Society of Mechanical Engineers

Paper No: GT2004-53199

https://doi.org/10.1115/GT2004-53199

View Paper titled, Numerical Prediction of Film Cooling and Heat Transfer With Different Film-Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade

Topics: Blades, Film cooling, Gas turbines, Heat transfer, Heat transfer coefficients, Leakage flows, Stress, Coolants, Equilibrium (Physics), Heat

Proceedings Papers

Film-Cooling Effectiveness on Squealer Rim Walls and Squealer Cavity Floor of a Gas Turbine Blade Tip Using Pressure Sensitive Paint

Shantanu Mhetras, Huitao Yang, Zhihong Gao, Je-Chin Han

Proc. ASME. GT2005, Volume 3: Turbo Expo 2005, Parts A and B, 397-408, June 6–9, 2005

Publisher: American Society of Mechanical Engineers

Paper No: GT2005-68387

https://doi.org/10.1115/GT2005-68387

View Paper titled, Film-Cooling Effectiveness on Squealer Rim Walls and Squealer Cavity Floor of a Gas Turbine Blade Tip Using Pressure Sensitive Paint

Topics: Blades, Cavities, Film cooling, Gas turbines, Paints, Pressure, Coolants, Cascades (Fluid dynamics), Nitrogen, Oxygen

Proceedings Papers

Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade With Two Rows Holes in a 1-1/2 Turbine Stage at Design and Off Design Conditions

Huitao Yang, Hamn-Ching Chen, Je-Chin Han, Hee-Koo Moon

Proc. ASME. GT2005, Volume 3: Turbo Expo 2005, Parts A and B, 335-344, June 6–9, 2005

Publisher: American Society of Mechanical Engineers

Paper No: GT2005-68335

https://doi.org/10.1115/GT2005-68335

View Paper titled, Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade With Two Rows Holes in a 1-1/2 Turbine Stage at Design and Off Design Conditions

Topics: Design, Film cooling, Heat transfer, Rotating blades, Turbines, Heat transfer coefficients, Pressure, Suction, Blades, Computer simulation

Proceedings Papers

Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows

Lesley M. Wright, Zhihong Gao, Huitao Yang, Je-Chin Han

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 383-394, May 8–11, 2006

Publisher: American Society of Mechanical Engineers

Paper No: GT2006-90375

https://doi.org/10.1115/GT2006-90375

View Paper titled, Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows

Topics: Blades, Film cooling, Flow (Dynamics), Gas turbines, Leakage, Coolants, Turbulence, Cooling, Rotors, Turbine blades

Proceedings Papers

Numerical Study of a Rotating Blade Platform With Film Cooling From Cavity Purge Flow in a 1-1/2 Turbine Stage

Huitao Yang, Hamn-Ching Chen, Je-Chin Han

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 315-324, May 8–11, 2006

Publisher: American Society of Mechanical Engineers

Paper No: GT2006-90322

https://doi.org/10.1115/GT2006-90322

View Paper titled, Numerical Study of a Rotating Blade Platform With Film Cooling From Cavity Purge Flow in a 1-1/2 Turbine Stage

Topics: Cavities, Film cooling, Flow (Dynamics), Rotating blades, Turbines, Coolants, Computer simulation, Engineering simulation, Equilibrium (Physics), Heat transfer coefficients

Journal Articles

Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows

Lesley M. Wright, Zhihong Gao, Huitao Yang, Je-Chin Han

Publisher: ASME

J. Heat Mass Transfer. July 2008, 130(7): 071702.

https://doi.org/10.1115/1.2907440

Published Online: May 19, 2008

View Article titled, Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows

Topics: Film cooling, Flow (Dynamics), Blades, Coolants, Cooling, Cascades (Fluid dynamics), Turbulence, Pressure

Proceedings Papers

Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade in a 1-1/2 Turbine Stage

Huitao Yang, Hamn-Ching Chen, Je-Chin Han, Hee-Koo Moon

Proc. ASME. IMECE2004, Heat Transfer, Volume 1, 555-564, November 13–19, 2004

Publisher: American Society of Mechanical Engineers

Paper No: IMECE2004-59599

https://doi.org/10.1115/IMECE2004-59599

View Paper titled, Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade in a 1-1/2 Turbine Stage

Topics: Film cooling, Heat transfer, Rotating blades, Turbines, Blades, Cooling, Stress, Computer simulation, Equilibrium (Physics), Gas turbines

Journal citation

NARROW

Heat Transfer and Pressure Drop Correlations for Square Channels With 45 Deg Ribs at High Reynolds Numbers

Flow and Heat Transfer Predictions for a Flat-Tip Turbine Blade

Numerical Simulation of Film Cooling on the Tip of a Gas Turbine Blade

Numerical Simulation of Flow and Heat Transfer Past a Turbine Blade With a Squealer-Tip

Numerical Study of Flow and Heat Transfer on a Blade Tip With Different Leakage Reduction Strategies

Numerical Prediction of Film Cooling and Heat Transfer With Different Film-Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade

Film-Cooling Effectiveness on Squealer Rim Walls and Squealer Cavity Floor of a Gas Turbine Blade Tip Using Pressure Sensitive Paint

Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade With Two Rows Holes in a 1-1/2 Turbine Stage at Design and Off Design Conditions

Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows

Numerical Study of a Rotating Blade Platform With Film Cooling From Cavity Purge Flow in a 1-1/2 Turbine Stage

Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows

Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade in a 1-1/2 Turbine Stage

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