Volume 113 Issue 3 | J. Turbomach. | ASME Digital Collection

Research Papers

Heat Transfer in Rotating Serpentine Passages With Smooth Walls

J. H. Wagner, B. V. Johnson, F. C. Kopper

J. Turbomach. July 1991, 113(3): 321–330. doi: https://doi.org/10.1115/1.2927879

View articletitled, Heat Transfer in Rotating Serpentine Passages With Smooth Walls

Topics: Heat transfer , Flow (Dynamics) , Buoyancy , Coolants , Heat transfer coefficients , Rotation , Turbine blades , Cooling , Coriolis force , Gas turbines

Parametric and Numerical Study of Fully Developed Flow and Heat Transfer in Rotating Rectangular Ducts

H. Iacovides, B. E. Launder

J. Turbomach. July 1991, 113(3): 331–338. doi: https://doi.org/10.1115/1.2927880

Abstract

View articletitled, Parametric and Numerical Study of Fully Developed Flow and Heat Transfer in Rotating Rectangular Ducts

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Topics: Ducts , Flow (Dynamics) , Heat transfer , Reynolds number , Pressure , Turbulence , Vortices , Suction , Computation , Cross section (Physics)

Heat Transfer Measurements in Rectangular Channels With Orthogonal Mode Rotation

W. D. Morris, G. Ghavami-Nasr

J. Turbomach. July 1991, 113(3): 339–345. doi: https://doi.org/10.1115/1.2927881

Abstract

View articletitled, Heat Transfer Measurements in Rectangular Channels With Orthogonal Mode Rotation

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Topics: Heat transfer , Rotation , Ducts , Flow (Dynamics) , Coolants , Blades , Buoyancy , Cooling , Forced convection , Gas turbines

An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened With 45 deg Criss-Cross Ribs on Two Opposite Walls

M. E. Taslim, L. A. Bondi, D. M. Kercher

J. Turbomach. July 1991, 113(3): 346–353. doi: https://doi.org/10.1115/1.2927882

Abstract

View articletitled, An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened With 45 deg Criss-Cross Ribs on Two Opposite Walls

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Topics: Heat transfer , Cooling , Rotation , Heat transfer coefficients , Blades , Circuits , Surface roughness , Turbine blades , Aircraft engines , Creep

An Investigation of Convective Heat Transfer in a Rotating Coolant Channel

J. O. Medwell, W. D. Morris, J. Y. Xia, C. Taylor

J. Turbomach. July 1991, 113(3): 354–359. doi: https://doi.org/10.1115/1.2927883

Abstract

View articletitled, An Investigation of Convective Heat Transfer in a Rotating Coolant Channel

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Topics: Convection , Coolants , Cooling , Ducts , Equations of motion , Finite element methods , Heat conduction , Heat transfer , Numerical analysis , Turbine blades

Turbulent Heat Transfer and Friction in a Square Channel With Discrete Rib Turbulators

S. C. Lau, R. D. McMillin, J. C. Han

J. Turbomach. July 1991, 113(3): 360–366. doi: https://doi.org/10.1115/1.2927884

Abstract

View articletitled, Turbulent Heat Transfer and Friction in a Square Channel With Discrete Rib Turbulators

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Topics: Friction , Turbulent heat transfer , Flow (Dynamics) , Heat transfer , Reynolds number , Turning

Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs

S. C. Lau, R. D. McMillin, J. C. Han

J. Turbomach. July 1991, 113(3): 367–374. doi: https://doi.org/10.1115/1.2927885

Abstract

View articletitled, Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs

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Topics: Heat transfer , Turbulence , Pressure drop , Airfoils , Cooling , Flow (Dynamics) , Friction , Gas turbines , Reynolds number , Turbulent heat transfer

Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade

A. Yamamoto, Y. Kondo, R. Murao

J. Turbomach. July 1991, 113(3): 375–383. doi: https://doi.org/10.1115/1.2927886

Abstract

View articletitled, Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade

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Topics: Cascades (Fluid dynamics) , Cooling , Flow (Dynamics) , Turbines , Blades , Internal flow , Kinetic energy , Turbine blades , Vortices

Heat Transfer and Aerodynamics of a High Rim Speed Turbine Nozzle Guide Vane Tested in the RAE Isentropic Light Piston Cascade (ILPC)

S. P. Harasgama, E. T. Wedlake

J. Turbomach. July 1991, 113(3): 384–391. doi: https://doi.org/10.1115/1.2927887

Abstract

View articletitled, Heat Transfer and Aerodynamics of a High Rim Speed Turbine Nozzle Guide Vane Tested in the RAE Isentropic Light Piston Cascade (ILPC)

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Topics: Aerodynamics , Cascades (Fluid dynamics) , Heat transfer , Nozzle guide vanes , Pistons , Turbines , Mach number , Reynolds number , Chords (Trusses) , Engines

Navier–Stokes Analysis of Turbine Blade Heat Transfer

R. J. Boyle

J. Turbomach. July 1991, 113(3): 392–403. doi: https://doi.org/10.1115/1.2927888

Abstract

View articletitled, Navier–Stokes Analysis of Turbine Blade Heat Transfer

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Topics: Heat transfer , Turbine blades , Turbulence , Blades , Eddies (Fluid dynamics) , Flow (Dynamics) , Prandtl number , Pressure gradient , Reynolds number , Turbines

Heat Transfer Measurements and Calculations in Transitionally Rough Flow

M. H. Hosni, H. W. Coleman, R. P. Taylor

J. Turbomach. July 1991, 113(3): 404–411. doi: https://doi.org/10.1115/1.2927889

Abstract

View articletitled, Heat Transfer Measurements and Calculations in Transitionally Rough Flow

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Topics: Flow (Dynamics) , Heat transfer , Surface roughness , Turbulence , Air flow , Boundary layer turbulence , Boundary layers , Computation , Pressure gradient , Skin friction (Fluid dynamics)

The Effect of Incident Wake Conditions on the Mean Heat Transfer of an Airfoil

K. Dullenkopf, A. Schulz, S. Wittig

J. Turbomach. July 1991, 113(3): 412–418. doi: https://doi.org/10.1115/1.2927890

Abstract

View articletitled, The Effect of Incident Wake Conditions on the Mean Heat Transfer of an Airfoil

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Topics: Airfoils , Heat transfer , Wakes , Cascades (Fluid dynamics) , Blades , Flow (Dynamics) , Boundary layers , Cylinders , Generators , Heat

Laminar Boundary Layer Interaction With an Unsteady Passing Wake

D. E. Paxson, R. E. Mayle

J. Turbomach. July 1991, 113(3): 419–427. doi: https://doi.org/10.1115/1.2927891

Abstract

View articletitled, Laminar Boundary Layer Interaction With an Unsteady Passing Wake

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Topics: Boundary layers , Wakes , Flow (Dynamics) , Oscillations

More on the Turbulent-Strip Theory for Wake-Induced Transition

R. E. Mayle, K. Dullenkopf

J. Turbomach. July 1991, 113(3): 428–432. doi: https://doi.org/10.1115/1.2927892

Abstract

View articletitled, More on the Turbulent-Strip Theory for Wake-Induced Transition

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Topics: Strips , Turbulence , Wakes , Flow (Dynamics) , Boundary layers , Dimensional analysis , Wake turbulence

Effects of Vortices With Different Circulations on Heat Transfer and Injectant Downstream of a Single Film-Cooling Hole in a Turbulent Boundary Layer

P. M. Ligrani, C. S. Subramanian, D. W. Craig, P. Kaisuwan

J. Turbomach. July 1991, 113(3): 433–441. doi: https://doi.org/10.1115/1.2927893

Abstract

View articletitled, Effects of Vortices With Different Circulations on Heat Transfer and Injectant Downstream of a Single Film-Cooling Hole in a Turbulent Boundary Layer

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Topics: Boundary layer turbulence , Film cooling , Heat transfer , Vortices , Flow (Dynamics) , Temperature , Boundary layers , Heat flux

Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio

A. K. Sinha, D. G. Bogard, M. E. Crawford

J. Turbomach. July 1991, 113(3): 442–449. doi: https://doi.org/10.1115/1.2927894

Abstract

View articletitled, Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio

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Topics: Density , Film cooling , Momentum , Jets , Temperature , Coolants , Errors , Heat conduction , Thermocouples

Gas Turbine Film Cooling: Flowfield Due to a Second Row of Holes

A. K. Sinha, D. G. Bogard, M. E. Crawford

J. Turbomach. July 1991, 113(3): 450–456. doi: https://doi.org/10.1115/1.2927895

Abstract

View articletitled, Gas Turbine Film Cooling: Flowfield Due to a Second Row of Holes

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Topics: Film cooling , Gas turbines , Boundary layers , Density , Jets , Shear stress , Turbulence

Velocity and Temperature Profiles for Stagnation Film Cooling

R. E. Mayle, A. Anderson

J. Turbomach. July 1991, 113(3): 457–463. doi: https://doi.org/10.1115/1.2927896

Abstract

View articletitled, Velocity and Temperature Profiles for Stagnation Film Cooling

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Topics: Film cooling , Temperature profiles , Flow (Dynamics) , Fluids , Temperature measurement

Effect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface

H. D. Ammari, N. Hay, D. Lampard

J. Turbomach. July 1991, 113(3): 464–471. doi: https://doi.org/10.1115/1.2927897

Abstract

View articletitled, Effect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface

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Topics: Heat transfer coefficients , Density , Carbon dioxide , Coolants , Flat plates , Mass transfer

The Influence of Curvature on Film Cooling Performance

S. G. Schwarz, R. J. Goldstein, E. R. G. Eckert

J. Turbomach. July 1991, 113(3): 472–478. doi: https://doi.org/10.1115/1.2927898

Abstract

View articletitled, The Influence of Curvature on Film Cooling Performance

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Topics: Film cooling , Momentum , Density , Flow (Dynamics) , Flow instability , Mass transfer , Pressure gradient

Film Cooling Effectiveness in High-Turbulence Flow

G. W. Jumper, W. C. Elrod, R. B. Rivir

J. Turbomach. July 1991, 113(3): 479–483. doi: https://doi.org/10.1115/1.2927899

Abstract

View articletitled, Film Cooling Effectiveness in High-Turbulence Flow

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Topics: Film cooling , Flow (Dynamics) , Turbulence , Reynolds number , Cooling , Ejectors , Flat plates

Film Cooling in the Presence of Mainstream Pressure Gradients

A. J. H. Teekaram, C. J. P. Forth, T. V. Jones

J. Turbomach. July 1991, 113(3): 484–492. doi: https://doi.org/10.1115/1.2927900

Abstract

View articletitled, Film Cooling in the Presence of Mainstream Pressure Gradients

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Topics: Film cooling , Pressure gradient , Boundary layer turbulence , Energy dissipation , Engines , Flat plates , Flow (Dynamics) , Gas turbines , Heat transfer coefficients , Mach number

Effect of Incidence on Wall Heating Rates and Aerodynamics on a Film-Cooled Transonic Turbine Blade

C. Camci, T. Arts

J. Turbomach. July 1991, 113(3): 493–501. doi: https://doi.org/10.1115/1.2927901

Abstract

View articletitled, Effect of Incidence on Wall Heating Rates and Aerodynamics on a Film-Cooled Transonic Turbine Blade

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Topics: Aerodynamics , Heating , Turbine blades , Cooling , Blades , Convection , Flow (Dynamics) , Heat transfer , Pressure , Suction

Turbine Tip and Shroud Heat Transfer

D. E. Metzger, M. G. Dunn, C. Hah

J. Turbomach. July 1991, 113(3): 502–507. doi: https://doi.org/10.1115/1.2927902

Abstract

View articletitled, Turbine Tip and Shroud Heat Transfer

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Topics: Heat transfer , Turbines , Blades , Leakage flows , Clearances (Engineering) , Pressure , Flow (Dynamics) , Airfoils , Computation , Cooling

Research Papers

Heat Transfer in Rotating Serpentine Passages With Smooth Walls

Parametric and Numerical Study of Fully Developed Flow and Heat Transfer in Rotating Rectangular Ducts

Heat Transfer Measurements in Rectangular Channels With Orthogonal Mode Rotation

An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened With 45 deg Criss-Cross Ribs on Two Opposite Walls

An Investigation of Convective Heat Transfer in a Rotating Coolant Channel

Turbulent Heat Transfer and Friction in a Square Channel With Discrete Rib Turbulators

Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs

Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade

Heat Transfer and Aerodynamics of a High Rim Speed Turbine Nozzle Guide Vane Tested in the RAE Isentropic Light Piston Cascade (ILPC)

Navier–Stokes Analysis of Turbine Blade Heat Transfer

Heat Transfer Measurements and Calculations in Transitionally Rough Flow

The Effect of Incident Wake Conditions on the Mean Heat Transfer of an Airfoil

Laminar Boundary Layer Interaction With an Unsteady Passing Wake

More on the Turbulent-Strip Theory for Wake-Induced Transition

Effects of Vortices With Different Circulations on Heat Transfer and Injectant Downstream of a Single Film-Cooling Hole in a Turbulent Boundary Layer

Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio

Gas Turbine Film Cooling: Flowfield Due to a Second Row of Holes

Velocity and Temperature Profiles for Stagnation Film Cooling

Effect of Acceleration on the Heat Transfer Coefficient on a Film-Cooled Surface

The Influence of Curvature on Film Cooling Performance

Film Cooling Effectiveness in High-Turbulence Flow

Film Cooling in the Presence of Mainstream Pressure Gradients

Effect of Incidence on Wall Heating Rates and Aerodynamics on a Film-Cooled Transonic Turbine Blade

Turbine Tip and Shroud Heat Transfer

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