The influence of wake-wake interactions on loss fluctuations of a downstream axial compressor blade row

The influence of blade stacking on turbine losses

Harrison, S

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D61039 / BLDSC - British Library Doc...

Investigation of Unsteady Flow Effects in an Axial Compressor Based on Whole Annulus Computations

Röber, Thomas
Kügeler, Edmund
Weber, Anton

January 2010

Flows in the ﬁrst stages of axial compressors are subject to a number of unsteady effects which are ...

A study of spike and modal stall phenomena in a low-speed axial compressor

Camp, T.
Day, I.
Rolls-Royce plc (United Kingdom)

January 1997

Available from British Library Document Supply Centre-DSC:8019.322(92341) / BLDSC - British Library ...

Wake-boundary layer interaction in axial flow turbomachinery

Addison, J.S

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D61318 / BLDSC - British Library Doc...

The influence of blade wakes on the peformance of inter-turbine diffusers

Dominy, R.
Kirkham, D
Rolls-Royce plc (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--92018) / BLDSC - B...

Blade Row Interaction Effects on the Performance of a Moderately Loaded NASA Transonic Compressor Stage

VanZante, Dale E.
To, Wai-Ming
Chen, Jen-Ping

March 2003

Blade row interaction effects on loss generation in compressors have received increased attention as...

INVESTIGATION OF INTERFERENCE INFLUENCE OF BLADE ROWS ON LOSSES IN AXIAL COMPRESSOR STAGE

Yuriy M. Tereshchenko
Ekaterina Doroshenko
Yuriy Yu. Tereshchenko
Pavel Gumenyuk

April 2018

Purpose: the purpose of this work is to investigate the total pressure losses in the input guide van...

The influence of turbulence on wake dispersion and blade row interaction in an axial compressor

Henderson, AD
Walker, GJ
Hughes, JD

January 2006

The influence of free-stream turbulence on wake dispersion and boundary layer transition processes h...

Significance of Compressor Blade Row Interactions on Loss Production Investigated

VanZante, Dale e.

March 2003

The performance of compressors and the sophistication of analysis tools have reached a level such th...

A study of the effect of wake passing on turbine blades

Doorly, D.J.

January 1983

SIGLELD:D50632/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Wake interaction effects on the transition process on turbine blades Final technical report 1 September - December 1988

Ainsworth, R.W.
LaGraff, J.E
Oxford Univ. (United Kingdom). Dept. of Engineering Science

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:0678.231F(AD-A--214492)(microfiche) ...

Unsteady aerodynamics in an axial flow compressor

Hughes, JD

January 2001

Current methods for designing compressor blades in axial turbomachines assume that the flow through ...

Blade tip clearance effects on an axial flow compressor rotor

Schmidt, M.J.P
Cranfield Inst. of Technology, Bedford (United Kingdom)

January 1985

SIGLEAvailable from British Library Lending Division - LD:D57590/85 / BLDSC - British Library Docume...

Periodic wake impingement and stall driving loss in axial compressors

Aldo Rona (7583084)
Jonathan Gostelow (8542602)
Motoyuki Kawase (7636412)

September 2018

Axial compressors are used in power generation and aircraft engines. In compressor design, three dim...

The effects of reaction on axial compressor performance

Farmakalides, C
Cranfield Inst. of Technology (United Kingdom)

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97979 / BLDSC - British Library Do...

The influence of blade stacking on turbine losses

Harrison, S

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D61039 / BLDSC - British Library Doc...

Investigation of Unsteady Flow Effects in an Axial Compressor Based on Whole Annulus Computations

Röber, Thomas
Kügeler, Edmund
Weber, Anton

January 2010

Flows in the ﬁrst stages of axial compressors are subject to a number of unsteady effects which are ...

A study of spike and modal stall phenomena in a low-speed axial compressor

Camp, T.
Day, I.
Rolls-Royce plc (United Kingdom)

January 1997

Available from British Library Document Supply Centre-DSC:8019.322(92341) / BLDSC - British Library ...

Wake-boundary layer interaction in axial flow turbomachinery

Addison, J.S

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:D61318 / BLDSC - British Library Doc...

The influence of blade wakes on the peformance of inter-turbine diffusers

Dominy, R.
Kirkham, D
Rolls-Royce plc (United Kingdom)

January 1994

SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RR-PNR--92018) / BLDSC - B...

Blade Row Interaction Effects on the Performance of a Moderately Loaded NASA Transonic Compressor Stage

VanZante, Dale E.
To, Wai-Ming
Chen, Jen-Ping

March 2003

Blade row interaction effects on loss generation in compressors have received increased attention as...

INVESTIGATION OF INTERFERENCE INFLUENCE OF BLADE ROWS ON LOSSES IN AXIAL COMPRESSOR STAGE

Yuriy M. Tereshchenko
Ekaterina Doroshenko
Yuriy Yu. Tereshchenko
Pavel Gumenyuk

April 2018

Purpose: the purpose of this work is to investigate the total pressure losses in the input guide van...

The influence of turbulence on wake dispersion and blade row interaction in an axial compressor

Henderson, AD
Walker, GJ
Hughes, JD

January 2006

The influence of free-stream turbulence on wake dispersion and boundary layer transition processes h...

Significance of Compressor Blade Row Interactions on Loss Production Investigated

VanZante, Dale e.

March 2003

The performance of compressors and the sophistication of analysis tools have reached a level such th...

A study of the effect of wake passing on turbine blades

Doorly, D.J.

January 1983

SIGLELD:D50632/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Wake interaction effects on the transition process on turbine blades Final technical report 1 September - December 1988

Ainsworth, R.W.
LaGraff, J.E
Oxford Univ. (United Kingdom). Dept. of Engineering Science

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:0678.231F(AD-A--214492)(microfiche) ...

Unsteady aerodynamics in an axial flow compressor

Hughes, JD

January 2001

Current methods for designing compressor blades in axial turbomachines assume that the flow through ...

Blade tip clearance effects on an axial flow compressor rotor

Schmidt, M.J.P
Cranfield Inst. of Technology, Bedford (United Kingdom)

January 1985

SIGLEAvailable from British Library Lending Division - LD:D57590/85 / BLDSC - British Library Docume...

Periodic wake impingement and stall driving loss in axial compressors

Aldo Rona (7583084)
Jonathan Gostelow (8542602)
Motoyuki Kawase (7636412)

September 2018

Axial compressors are used in power generation and aircraft engines. In compressor design, three dim...

The effects of reaction on axial compressor performance

Farmakalides, C
Cranfield Inst. of Technology (United Kingdom)

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:DX97979 / BLDSC - British Library Do...

The influence of blade stacking on turbine losses

Harrison, S

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:D61039 / BLDSC - British Library Doc...

Investigation of Unsteady Flow Effects in an Axial Compressor Based on Whole Annulus Computations

Röber, Thomas
Kügeler, Edmund
Weber, Anton

January 2010

Flows in the ﬁrst stages of axial compressors are subject to a number of unsteady effects which are ...

A study of spike and modal stall phenomena in a low-speed axial compressor

Camp, T.
Day, I.
Rolls-Royce plc (United Kingdom)

January 1997

Available from British Library Document Supply Centre-DSC:8019.322(92341) / BLDSC - British Library ...

The influence of wake-wake interactions on loss fluctuations of a downstream axial compressor blade row

Abstract

Extracted data

The influence of wake-wake interactions on loss fluctuations of a downstream axial compressor blade row

Abstract

Extracted data

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