The fluid mechanic of impingement and film cooling holes for turbine blade leading edges

Experimental and Numerical Investigation of Turbine Blade Leading Edge Heat Transfer with Jet Impingement and Film Cooling

Zhang, Mingjie

January 2019

Modern gas turbines engines are designed with higher turbine inlet temperatures to increase the over...

Turbine Blade Internal Heat Transfer and Film Cooling Studies

Wang, Nian

January 2019

Gas turbine engines are widely used in many industrial applications including aircraft propulsion, l...

AFIT/GAE/ENY/09-D01 Flow Visualization Study of Passive Flow Control Features On a Film-Cooled Turbine Blade Leading Edge

Daniel R. Carroll
Daniel R. Carroll

January 2009

A flow visualization study was conducted on a model of a film-cooled turbine blade leading edge in a...

Heat transfer near the entrance to a film cooling hole in a gas turbine blade

Byerley, A.R

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D89393 / BLDSC - British Library Doc...

The technical development of cooled gas turbine blades

Robbins, S.H.
Tubbs, H
Rolls-Royce Ltd., Derby (United Kingdom)

January 1985

SIGLEAvailable from British Library Lending Division - LD:8019.3153(PNR--90292) / BLDSC - British Li...

Internal cooling of turbine blades

Ireland, P

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D90175 / BLDSC - British Library Doc...

Mathematical models for a fluid flow arising in turbine blade cooling passages

Morland, L.C

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:D89429 / BLDSC - British Library Doc...

Turbine rotor blade erosion control with film cooling

Al-Hassani, T
Cranfield Inst. of Tech. (United Kingdom)

January 1982

SIGLEAvailable from British Library Document Supply Centre- DSC:D43828/82 / BLDSC - British Library ...

A study of flow and heat transfer in gas turbine blade cooling passages

Dunne, S.T.

January 1983

SIGLELD:D49851/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Numerical investigation of film and impingement cooling schemes for gas turbine application

Da Silva, Lucilene Moraes
Tomita, Jesuino Takachi
Bringhenti, Cleverson
Gr\uf6nstedt, Tomas

January 2018

In modern gas turbine engines, many sophisticated cooling schemes are used to maintain the turbine b...

Aerodynamics of an annular film-cooled turbine cascade

Day, C.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D196444 / BLDSC - British Library Doc...

Aerodynamics and heat transfer of turbine blading

Horton, F.G

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:D73493/87 / BLDSC - British Library ...

Development of a novel film cooling hole geometry

Sargison, J.E.

January 2001

Available from British Library Document Supply Centre-DSC:D213879 / BLDSC - British Library Document...

Discharge coefficients of nozzle guide vane film cooling holes

Rowbury, D.

January 1998

Available from British Library Document Supply Centre-DSC:D213668 / BLDSC - British Library Document...

Aerodynamics of turbine rim-seal ingestion

Hills, N.J.
Green, T.
Turner, A.B.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92310) / BLDSC - British Lib...

Experimental and Numerical Investigation of Turbine Blade Leading Edge Heat Transfer with Jet Impingement and Film Cooling

Zhang, Mingjie

January 2019

Modern gas turbines engines are designed with higher turbine inlet temperatures to increase the over...

Turbine Blade Internal Heat Transfer and Film Cooling Studies

Wang, Nian

January 2019

Gas turbine engines are widely used in many industrial applications including aircraft propulsion, l...

AFIT/GAE/ENY/09-D01 Flow Visualization Study of Passive Flow Control Features On a Film-Cooled Turbine Blade Leading Edge

Daniel R. Carroll
Daniel R. Carroll

January 2009

A flow visualization study was conducted on a model of a film-cooled turbine blade leading edge in a...

Heat transfer near the entrance to a film cooling hole in a gas turbine blade

Byerley, A.R

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D89393 / BLDSC - British Library Doc...

The technical development of cooled gas turbine blades

Robbins, S.H.
Tubbs, H
Rolls-Royce Ltd., Derby (United Kingdom)

January 1985

SIGLEAvailable from British Library Lending Division - LD:8019.3153(PNR--90292) / BLDSC - British Li...

Internal cooling of turbine blades

Ireland, P

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D90175 / BLDSC - British Library Doc...

Mathematical models for a fluid flow arising in turbine blade cooling passages

Morland, L.C

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:D89429 / BLDSC - British Library Doc...

Turbine rotor blade erosion control with film cooling

Al-Hassani, T
Cranfield Inst. of Tech. (United Kingdom)

January 1982

SIGLEAvailable from British Library Document Supply Centre- DSC:D43828/82 / BLDSC - British Library ...

A study of flow and heat transfer in gas turbine blade cooling passages

Dunne, S.T.

January 1983

SIGLELD:D49851/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Numerical investigation of film and impingement cooling schemes for gas turbine application

Da Silva, Lucilene Moraes
Tomita, Jesuino Takachi
Bringhenti, Cleverson
Gr\uf6nstedt, Tomas

January 2018

In modern gas turbine engines, many sophisticated cooling schemes are used to maintain the turbine b...

Aerodynamics of an annular film-cooled turbine cascade

Day, C.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D196444 / BLDSC - British Library Doc...

Aerodynamics and heat transfer of turbine blading

Horton, F.G

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:D73493/87 / BLDSC - British Library ...

Development of a novel film cooling hole geometry

Sargison, J.E.

January 2001

Available from British Library Document Supply Centre-DSC:D213879 / BLDSC - British Library Document...

Discharge coefficients of nozzle guide vane film cooling holes

Rowbury, D.

January 1998

Available from British Library Document Supply Centre-DSC:D213668 / BLDSC - British Library Document...

Aerodynamics of turbine rim-seal ingestion

Hills, N.J.
Green, T.
Turner, A.B.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92310) / BLDSC - British Lib...

Experimental and Numerical Investigation of Turbine Blade Leading Edge Heat Transfer with Jet Impingement and Film Cooling

Zhang, Mingjie

January 2019

Modern gas turbines engines are designed with higher turbine inlet temperatures to increase the over...

Turbine Blade Internal Heat Transfer and Film Cooling Studies

Wang, Nian

January 2019

Gas turbine engines are widely used in many industrial applications including aircraft propulsion, l...

AFIT/GAE/ENY/09-D01 Flow Visualization Study of Passive Flow Control Features On a Film-Cooled Turbine Blade Leading Edge

Daniel R. Carroll
Daniel R. Carroll

January 2009

A flow visualization study was conducted on a model of a film-cooled turbine blade leading edge in a...

The fluid mechanic of impingement and film cooling holes for turbine blade leading edges

Abstract

Extracted data

The fluid mechanic of impingement and film cooling holes for turbine blade leading edges

Abstract

Extracted data

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