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Journal Articles

Boundary Layer Flashback Model for Hydrogen Flames in Confined Geometries Including the Effect of Adverse Pressure Gradient

Ólafur H. Björnsson, Sikke A. Klein, Joeri Tober

J. Eng. Gas Turbines Power. June 2021, 143(6): 061003.

Paper No: GTP-20-1415

https://doi.org/10.1115/1.4048566

Published Online: March 15, 2021

View Article titled, Boundary Layer Flashback Model for Hydrogen Flames in Confined Geometries Including the Effect of Adverse Pressure Gradient

Topics: Boundary layers, Flames, Flow (Dynamics), Pressure gradient, Hydrogen, Diffusers, Turbulence

Journal Articles

Flow Control in an Aggressive Interturbine Transition Duct Using Low Profile Vortex Generators

Yanfeng Zhang, Shuzhen Hu, Xue-Feng Zhang, Michael Benner, Ali Mahallati, Edward Vlasic

J. Eng. Gas Turbines Power. November 2014, 136(11): 112604.

Paper No: GTP-13-1010

https://doi.org/10.1115/1.4027656

Published Online: June 3, 2014

View Article titled, Flow Control in an Aggressive Interturbine Transition Duct Using Low Profile Vortex Generators

Topics: Boundary layers, Ducts, Flow (Dynamics), Flow control, Generators, Pressure, Separation (Technology), Vortices, Wakes, Vorticity

Journal Articles

Effect of Void Fraction on Pressure Drop in Upward Vertical Two-Phase Gas-Liquid Pipe Flow

Clement C. Tang, Sanjib Tiwari, Afshin J. Ghajar

J. Eng. Gas Turbines Power. February 2013, 135(2): 022901.

Paper No: GTP-12-1356

https://doi.org/10.1115/1.4007762

Published Online: January 8, 2013

View Article titled, Effect of Void Fraction on Pressure Drop in Upward Vertical Two-Phase Gas-Liquid Pipe Flow

Topics: Flow (Dynamics), Porosity, Pressure drop, Two-phase flow, Water, Pressure gradient

Journal Articles

The Importance of Circumferential Non-uniformities in a Passage-Averaged Quasi-Three-Dimensional Turbomachinery Design System

I. K. Jennions, P. Stow

J. Eng. Gas Turbines Power. April 1986, 108(2): 240–245.

https://doi.org/10.1115/1.3239894

Published Online: April 1, 1986

View Article titled, The Importance of Circumferential Non-uniformities in a Passage-Averaged Quasi-Three-Dimensional Turbomachinery Design System

Topics: Design, Turbomachinery, Blades, Pressure gradient, Rotors, Flow (Dynamics), Mathematical analysis, Nozzle guide vanes, Turbines

Journal Articles

Pressure Loss Due to the Tip Clearance of Impeller Blades in Centrifugal and Axial Blowers

Y. Senoo, M. Ishida

J. Eng. Gas Turbines Power. January 1986, 108(1): 32–37.

https://doi.org/10.1115/1.3239882

Published Online: January 1, 1986

View Article titled, Pressure Loss Due to the Tip Clearance of Impeller Blades in Centrifugal and Axial Blowers

Topics: Blades, Clearances (Engineering), Impellers, Pressure, Fluids, Leakage flows, Pressure gradient

Journal Articles

Calculation of Heat Transfer to Convection-Cooled Gas Turbine Blades

W. Rodi, G. Scheuerer

J. Eng. Gas Turbines Power. July 1985, 107(3): 620–627.

https://doi.org/10.1115/1.3239781

Published Online: July 1, 1985

View Article titled, Calculation of Heat Transfer to Convection-Cooled Gas Turbine Blades

Topics: Blades, Convection, Gas turbines, Heat transfer, Turbulence, Boundary layers, Flow (Dynamics), Heat transfer coefficients, Boundary-value problems, Computational methods

Journal Articles

The Transpired Turbulent Boundary Layer in Various Pressure Gradients and the Blow-Off Condition

D. P. Georgiou, J. F. Louis

J. Eng. Gas Turbines Power. July 1985, 107(3): 636–641.

https://doi.org/10.1115/1.3239783

Published Online: July 1, 1985

View Article titled, The Transpired Turbulent Boundary Layer in Various Pressure Gradients and the Blow-Off Condition

Topics: Boundary layer turbulence, Pressure gradient, Boundary layers, Cooling, Gas turbines, Heat transfer, Transpiration, Coolants, Flow (Dynamics), Reynolds number

Journal Articles

An Experimental Study of the Compressor Rotor Blade Boundary Layer

M. Pouagare, J. M. Galmes, B. Lakshminarayana

J. Eng. Gas Turbines Power. April 1985, 107(2): 364–372.

https://doi.org/10.1115/1.3239731

Published Online: April 1, 1985

View Article titled, An Experimental Study of the Compressor Rotor Blade Boundary Layer

Topics: Blades, Boundary layers, Compressors, Rotors, Annulus, Axial flow, Boundary layer turbulence, Cascades (Fluid dynamics), Leakage flows, Pressure gradient

Journal Articles

Effects of Cooling Films on the Heat Transfer Coefficient on a Flat Plate With Zero Mainstream Pressure Gradient

N. Hay, D. Lampard, C. L. Saluja

J. Eng. Gas Turbines Power. January 1985, 107(1): 105–110.

https://doi.org/10.1115/1.3239667

Published Online: January 1, 1985

View Article titled, Effects of Cooling Films on the Heat Transfer Coefficient on a Flat Plate With Zero Mainstream Pressure Gradient

Topics: Cooling, Flat plates, Heat transfer coefficients, Pressure gradient, Heat, Holographic interferometry, Lasers, Polymers

Journal Articles

Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces

K. Rued, S. Wittig

J. Eng. Gas Turbines Power. January 1985, 107(1): 54–59.

https://doi.org/10.1115/1.3239697

Published Online: January 1, 1985

View Article titled, Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces

Topics: Boundary layers, Heat transfer, Pressure gradient, Turbulence, Cooling, Boundary layer turbulence, Flat plates, Flow (Dynamics)

Journal Articles

Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces

N. Hay, D. Lampard, C. L. Saluja

J. Eng. Gas Turbines Power. January 1985, 107(1): 99–104.

https://doi.org/10.1115/1.3239703

Published Online: January 1, 1985

View Article titled, Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces

Topics: Boundary layers, Heat transfer coefficients, Pressure gradient, Flat plates, Heat

Journal Articles

Film Cooling From Two Rows of Holes Inclined in the Streamwise and Spanwise Directions

B. Jubran, A. Brown

J. Eng. Gas Turbines Power. January 1985, 107(1): 84–91.

https://doi.org/10.1115/1.3239701

Published Online: January 1, 1985

View Article titled, Film Cooling From Two Rows of Holes Inclined in the Streamwise and Spanwise Directions

Topics: Film cooling, Pressure gradient, Turbulence

Journal Articles

Modeling of Three-Dimensional Flow in Turning Channels

I. M. Khalil, H. G. Weber

J. Eng. Gas Turbines Power. July 1984, 106(3): 682–691.

https://doi.org/10.1115/1.3239624

Published Online: July 1, 1984

View Article titled, Modeling of Three-Dimensional Flow in Turning Channels

Topics: Flow (Dynamics), Modeling, Turning, Centrifugal force, Dimensions, Fluids, Laminar flow, Momentum, Navier-Stokes equations, Pressure gradient

Journal Articles

An Experimental Investigation of Endwall Heat Transfer and Aerodynamics in a Linear Vane Cascade

R. E. York, L. D. Hylton, M. S. Mihelc

J. Eng. Gas Turbines Power. January 1984, 106(1): 159–167.

https://doi.org/10.1115/1.3239529

Published Online: January 1, 1984

View Article titled, An Experimental Investigation of Endwall Heat Transfer and Aerodynamics in a Linear Vane Cascade

Topics: Aerodynamics, Cascades (Fluid dynamics), Heat transfer, Databases, Boundary layers, Cooling, Engines, Gas turbines, Heat flux, Mach number

Journal Articles

Investigation of the Laminar-Turbulent Transition of Boundary Layers Disturbed by Wakes

H. Pfeil, R. Herbst, T. Schro¨der

J. Eng. Gas Turbines Power. January 1983, 105(1): 130–137.

https://doi.org/10.1115/1.3227373

Published Online: January 1, 1983

View Article titled, Investigation of the Laminar-Turbulent Transition of Boundary Layers Disturbed by Wakes

Topics: Boundary layers, Turbulence, Wakes, Engineering drawings, Pressure gradient, Turbomachinery

Journal Articles

Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients

M. F. Blair

J. Eng. Gas Turbines Power. October 1982, 104(4): 743–750.

https://doi.org/10.1115/1.3227340

Published Online: October 1, 1982

View Article titled, Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients

Topics: Boundary layers, Pressure gradient, Turbulence, Heat transfer, Flow (Dynamics), Boundary layer turbulence, Reynolds number, Shapes, Temperature profiles

Journal Articles

Development of a Large-Scale Wind Tunnel for the Simulation of Turbomachinery Airfoil Boundary Layers

M. F. Blair, D. A. Bailey, R. H. Schlinker

J. Eng. Gas Turbines Power. October 1981, 103(4): 678–687.

https://doi.org/10.1115/1.3230790

Published Online: October 1, 1981

View Article titled, Development of a Large-Scale Wind Tunnel for the Simulation of Turbomachinery Airfoil Boundary Layers

Topics: Airfoils, Boundary layers, Simulation, Turbomachinery, Wind tunnels, Turbulence, Flow (Dynamics), Tunnels, Heat transfer, Pressure gradient

Journal Articles

On the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers

M. Ishida, Y. Senoo

J. Eng. Gas Turbines Power. April 1981, 103(2): 271–278.

https://doi.org/10.1115/1.3230717

Published Online: April 1, 1981

View Article titled, On the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers

Topics: Clearances (Engineering), Pressure, Impellers, Pressure gradient, Flow (Dynamics)

Journal Articles

Mean Velocity and Decay Characteristics of the Guidevane and Stator Blade Wake of an Axial Flow Compressor

B. Lakshminarayana, R. Davino

J. Eng. Gas Turbines Power. January 1980, 102(1): 50–60.

https://doi.org/10.1115/1.3230231

Published Online: January 1, 1980

View Article titled, Mean Velocity and Decay Characteristics of the Guidevane and Stator Blade Wake of an Axial Flow Compressor

Topics: Axial flow, Blades, Stators, Wakes, Inlet guide vanes, Compressors, Centrifugal force, Flow (Dynamics), Noise (Sound), Pressure gradient

Journal Articles

Use of the Characteristic Method for the Prediction of the Three-Dimensional Flow Field in High Transonic Compressors

J. Martinon

J. Eng. Gas Turbines Power. January 1980, 102(1): 96–103.

https://doi.org/10.1115/1.3230240

Published Online: January 1, 1980

View Article titled, Use of the Characteristic Method for the Prediction of the Three-Dimensional Flow Field in High Transonic Compressors

Topics: Compressors, Flow (Dynamics), Blades, Cascades (Fluid dynamics), Axial flow, Pressure gradient

Journal citation

NARROW

Boundary Layer Flashback Model for Hydrogen Flames in Confined Geometries Including the Effect of Adverse Pressure Gradient

Flow Control in an Aggressive Interturbine Transition Duct Using Low Profile Vortex Generators

Effect of Void Fraction on Pressure Drop in Upward Vertical Two-Phase Gas-Liquid Pipe Flow

The Importance of Circumferential Non-uniformities in a Passage-Averaged Quasi-Three-Dimensional Turbomachinery Design System

Pressure Loss Due to the Tip Clearance of Impeller Blades in Centrifugal and Axial Blowers

Calculation of Heat Transfer to Convection-Cooled Gas Turbine Blades

The Transpired Turbulent Boundary Layer in Various Pressure Gradients and the Blow-Off Condition

An Experimental Study of the Compressor Rotor Blade Boundary Layer

Effects of Cooling Films on the Heat Transfer Coefficient on a Flat Plate With Zero Mainstream Pressure Gradient

Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces

Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces

Film Cooling From Two Rows of Holes Inclined in the Streamwise and Spanwise Directions

Modeling of Three-Dimensional Flow in Turning Channels

An Experimental Investigation of Endwall Heat Transfer and Aerodynamics in a Linear Vane Cascade

Investigation of the Laminar-Turbulent Transition of Boundary Layers Disturbed by Wakes

Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients

Development of a Large-Scale Wind Tunnel for the Simulation of Turbomachinery Airfoil Boundary Layers

On the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers

Mean Velocity and Decay Characteristics of the Guidevane and Stator Blade Wake of an Axial Flow Compressor

Use of the Characteristic Method for the Prediction of the Three-Dimensional Flow Field in High Transonic Compressors

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