An investigation of boundary layer development in a multistage LP turbine

Boundary layer development on a nacelle afterbody

Lai, E
Cambridge Univ. (United Kingdom)

January 1983

SIGLEAvailable from British Library Lending Division - LD:D55328/85 / BLDSC - British Library Docume...

Aerodynamics of high performance turbine blading

King, P.I

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D69032/86 / BLDSC - British Library ...

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...

Boundary layer transition in simulated turbine blade flow

Graham, D
Dundee Institute of Technology (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX94436 / BLDSC - British Library Do...

Investigation of boundary layer development in a multistage LP turbine

Hodson, HP
Huntsman, I
Steele, AB
,

January 1993

This paper describes an investigation of the behavior of suction surface boundary layers in a modern...

An investigation of boundary layer development in a multistage LP turbine

Hodson, HP
Huntsman, I
Steele, AB
,

January 1994

This paper describes an investigation of the behavior of suction surface boundary layers in a modern...

An Investigation of Boundary Layer Development in a Multistage LP Turbine

H. P. Hodson
I. Huntsman
A. B. Steele

January 1994

The Society shall not be responsible for statements or opinions advanced in papers or discussion at ...

Separation of the boundary-layer as occuring on turbo-machinery blading

Yousif, A.H.

January 1982

SIGLELD:D47772/83 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

The aerodynamics of shrouded multistage turbines

Lewis, K.L.

January 1993

SIGLEAvailable from British Library Document Supply Centre-DSC:D063469 / BLDSC - British Library Doc...

Boundary layers on compressor blades

Dong, Y

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:D60095 / BLDSC - British Library Doc...

Transisiton to turbulance in the boundary layer of turbomachinery blading

Kalfas, A

January 1994

SIGLEAvailable from British Library Document Supply Centre-DSC:DX191593 / BLDSC - British Library Do...

Relaminarisation of turbulent boundary layers

Brandt, R.

January 1993

SIGLEAvailable from British Library Document Supply Centre-DSC:D063487 / BLDSC - British Library Doc...

Investigation of the aerodynamics and cooling of advance engine turbine components

Rose, M.
Sieverding, C.
Charna, K
Rolls-Royce plc (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--92041) / BLDSC - B...

Theoretical and experimental study of turbine flowmeters

Xu, Y
Cranfield Inst. of Technology (United Kingdom)

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX98007 / BLDSC - British Library Do...

Development of blade profiles for low pressure turbine applications

Curtis, E.
Hodson, H.
Banieghbal, M.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92315) / BLDSC - British Lib...

Boundary layer development on a nacelle afterbody

Lai, E
Cambridge Univ. (United Kingdom)

January 1983

SIGLEAvailable from British Library Lending Division - LD:D55328/85 / BLDSC - British Library Docume...

Aerodynamics of high performance turbine blading

King, P.I

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D69032/86 / BLDSC - British Library ...

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...

Boundary layer transition in simulated turbine blade flow

Graham, D
Dundee Institute of Technology (United Kingdom)
Council for National Academic Awards (CNAA), London (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX94436 / BLDSC - British Library Do...

Investigation of boundary layer development in a multistage LP turbine

Hodson, HP
Huntsman, I
Steele, AB
,

January 1993

This paper describes an investigation of the behavior of suction surface boundary layers in a modern...

An investigation of boundary layer development in a multistage LP turbine

Hodson, HP
Huntsman, I
Steele, AB
,

January 1994

This paper describes an investigation of the behavior of suction surface boundary layers in a modern...

An Investigation of Boundary Layer Development in a Multistage LP Turbine

H. P. Hodson
I. Huntsman
A. B. Steele

January 1994

The Society shall not be responsible for statements or opinions advanced in papers or discussion at ...

Separation of the boundary-layer as occuring on turbo-machinery blading

Yousif, A.H.

January 1982

SIGLELD:D47772/83 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

The aerodynamics of shrouded multistage turbines

Lewis, K.L.

January 1993

SIGLEAvailable from British Library Document Supply Centre-DSC:D063469 / BLDSC - British Library Doc...

Boundary layers on compressor blades

Dong, Y

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:D60095 / BLDSC - British Library Doc...

Transisiton to turbulance in the boundary layer of turbomachinery blading

Kalfas, A

January 1994

SIGLEAvailable from British Library Document Supply Centre-DSC:DX191593 / BLDSC - British Library Do...

Relaminarisation of turbulent boundary layers

Brandt, R.

January 1993

SIGLEAvailable from British Library Document Supply Centre-DSC:D063487 / BLDSC - British Library Doc...

Investigation of the aerodynamics and cooling of advance engine turbine components

Rose, M.
Sieverding, C.
Charna, K
Rolls-Royce plc (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--92041) / BLDSC - B...

Theoretical and experimental study of turbine flowmeters

Xu, Y
Cranfield Inst. of Technology (United Kingdom)

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX98007 / BLDSC - British Library Do...

Development of blade profiles for low pressure turbine applications

Curtis, E.
Hodson, H.
Banieghbal, M.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92315) / BLDSC - British Lib...

Boundary layer development on a nacelle afterbody

Lai, E
Cambridge Univ. (United Kingdom)

January 1983

SIGLEAvailable from British Library Lending Division - LD:D55328/85 / BLDSC - British Library Docume...

Aerodynamics of high performance turbine blading

King, P.I

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D69032/86 / BLDSC - British Library ...

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...

An investigation of boundary layer development in a multistage LP turbine

Abstract

Extracted data

An investigation of boundary layer development in a multistage LP turbine

Abstract

Extracted data

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