Discharge coefficients of nozzle guide vane film cooling holes

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

Chu, T.

January 1981

SIGLELD:D48743/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

GT2003-38252 COMPUTATIONAL PREDICTIONS OF ENDWALL FILM-COOLING FOR A FIRST STAGE VANE

Daniel G. Knost
Karen A. Thole

January 2016

In gas turbine development, the direction has been higher turbine inlet temperatures to increase the...

Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane

Hussain, Safeer
Liu, Jian
Sundén, Bengt

January 2020

The film cooling and heat transfer on the endwall especially in the junction region of a vane/blade ...

Discharge coefficient of film cooling holes with rounded entries or exits

Khaldi, A

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D80505 / BLDSC - British Library Doc...

Heat transfer on nozzle guide vane end walls

Harvey, N.W

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:D79821 / BLDSC - British Library Doc...

Heat transfer and aerodynamic studies of a nozzle guide vane and the development of new heat transfer gauges

Guo, S.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D198191 / BLDSC - British Library Doc...

Efficiency measurement of an annular nozzle guide vane cascade with different film cooling geometries

Day, C.
Oldfield, M.
Lock, G.
Rolls-Royce plc (United Kingdom)

January 1998

Paper submitted for ASME Turbo Expo 1998, StockholmAvailable from British Library Document Supply Ce...

Scaling of film cooling discharge coefficient measurement to engine conditions

Oldfield, M.
Lock, G.
Rowbury, D.
Rolls-Royce plc (United Kingdom)

January 1998

Available from British Library Document Supply Centre-DSC:8019.322(92467) / BLDSC - British Library ...

A METHOD FOR CORRELATING THE INFLUENCE OF EXTERNAL CROSSFLOW ON THE DISCHARGE COEFFICIENTS OF FILM COOLING HOLES

Asme/Igti Turbo Proceedings Of
Expo

April 2020

ABSTRACT An empirical means of predicting the discharge coefficients of film cooling holes in an ope...

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...

Measurement and calculation of nozzle guide vane end wall heat transfer

Harvey, N.
Rase, M.
Coupland, J.
Rolls-Royce plc (United Kingdom)

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92471) / BLDSC - British Lib...

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...

Detailed heat transfer measurements in nozzle guide vane passages in linear and annular cascades in the presence of secondary flows

Harvey, N
Rolls-Royce plc. (United Kingdom)

January 1989

Available from British Library Document Supply Centre- DSC:8019.3153(RRR-PNR--90706) / BLDSC - Briti...

Film cooling from two rows of holes in the streamwise and spanwise directions

Jubran, B

January 1984

Available from British Library Document Supply Centre- DSC:D52361/84 / BLDSC - British Library Docum...

THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS Discharge Coefficients of Impingement and Film Cooling Holes

Dr Tay Chu
Mr S Garrett

April 2020

ABSTRACT In this article measurements of fluid flow through impingement and film cooling holes for t...

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

Chu, T.

January 1981

SIGLELD:D48743/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

GT2003-38252 COMPUTATIONAL PREDICTIONS OF ENDWALL FILM-COOLING FOR A FIRST STAGE VANE

Daniel G. Knost
Karen A. Thole

January 2016

In gas turbine development, the direction has been higher turbine inlet temperatures to increase the...

Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane

Hussain, Safeer
Liu, Jian
Sundén, Bengt

January 2020

The film cooling and heat transfer on the endwall especially in the junction region of a vane/blade ...

Discharge coefficient of film cooling holes with rounded entries or exits

Khaldi, A

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:D80505 / BLDSC - British Library Doc...

Heat transfer on nozzle guide vane end walls

Harvey, N.W

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:D79821 / BLDSC - British Library Doc...

Heat transfer and aerodynamic studies of a nozzle guide vane and the development of new heat transfer gauges

Guo, S.

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:D198191 / BLDSC - British Library Doc...

Efficiency measurement of an annular nozzle guide vane cascade with different film cooling geometries

Day, C.
Oldfield, M.
Lock, G.
Rolls-Royce plc (United Kingdom)

January 1998

Paper submitted for ASME Turbo Expo 1998, StockholmAvailable from British Library Document Supply Ce...

Scaling of film cooling discharge coefficient measurement to engine conditions

Oldfield, M.
Lock, G.
Rowbury, D.
Rolls-Royce plc (United Kingdom)

January 1998

Available from British Library Document Supply Centre-DSC:8019.322(92467) / BLDSC - British Library ...

A METHOD FOR CORRELATING THE INFLUENCE OF EXTERNAL CROSSFLOW ON THE DISCHARGE COEFFICIENTS OF FILM COOLING HOLES

Asme/Igti Turbo Proceedings Of
Expo

April 2020

ABSTRACT An empirical means of predicting the discharge coefficients of film cooling holes in an ope...

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...

Measurement and calculation of nozzle guide vane end wall heat transfer

Harvey, N.
Rase, M.
Coupland, J.
Rolls-Royce plc (United Kingdom)

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92471) / BLDSC - British Lib...

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...

Detailed heat transfer measurements in nozzle guide vane passages in linear and annular cascades in the presence of secondary flows

Harvey, N
Rolls-Royce plc. (United Kingdom)

January 1989

Available from British Library Document Supply Centre- DSC:8019.3153(RRR-PNR--90706) / BLDSC - Briti...

Film cooling from two rows of holes in the streamwise and spanwise directions

Jubran, B

January 1984

Available from British Library Document Supply Centre- DSC:D52361/84 / BLDSC - British Library Docum...

THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS Discharge Coefficients of Impingement and Film Cooling Holes

Dr Tay Chu
Mr S Garrett

April 2020

ABSTRACT In this article measurements of fluid flow through impingement and film cooling holes for t...

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

Chu, T.

January 1981

SIGLELD:D48743/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

GT2003-38252 COMPUTATIONAL PREDICTIONS OF ENDWALL FILM-COOLING FOR A FIRST STAGE VANE

Daniel G. Knost
Karen A. Thole

January 2016

In gas turbine development, the direction has been higher turbine inlet temperatures to increase the...

Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane

Hussain, Safeer
Liu, Jian
Sundén, Bengt

January 2020

The film cooling and heat transfer on the endwall especially in the junction region of a vane/blade ...

Discharge coefficients of nozzle guide vane film cooling holes

Abstract

Extracted data

Discharge coefficients of nozzle guide vane film cooling holes

Abstract

Extracted data

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