Wake-boundary layer interaction in axial flow turbomachinery

Models for unsteady wake-induced transition in axial turbomachines

H. P. Hodson
J. S. Addison
C. A. Shepherson

January 1992

In turbomachinery, a considerable proportion of the blade surface area can be covered transitional b...

A study of unsteady wake-boundary layer interaction in turbomachines

Gete, Zenebe

January 1996

The relative motions of rotor and stator blade rows in a turbomachine generate periodically unstead...

Turbulence and complex flow phenomena in multi-stage axial turbomachines /

Katz, Joseph, author.
Meneveau, Charles, 1960-, author.
Johns Hopkins University, sponsor.
United States. Air Force. Office of Scientific Research, issuing body.

The objective of this project is to measure the flow within axial turbomachines and use the data to ...

Unsteady separated boundary layers in axial-flow turbomachinery

Schulte, V.

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:D197438 / BLDSC - British Library Doc...

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

Walker, G.
Hughes, J.
Koehler, I.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92339) / BLDSC - British Lib...

Three-dimensional interaction of wakes and boundary layers

Moghadam, A.H.K

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D59345 / BLDSC - British Library Doc...

A numerical study of the transonic blade-vortex interaction

Ng, N.L.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN027361 / BLDSC - British Library D...

An investigation into the unsteady blade interaction in one and a half stage axial flow turbine

Miller, R.J.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:D203928 / BLDSC - British Library Doc...

The interaction of a 2D turbulent wake with a bluff body

Ramsay, S.R

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:D60197 / BLDSC - British Library Doc...

Three-dimensional interaction of wake/boundary-layer and vortex/boundary-layer Data report

Yeung, C.
Squire, L
Cambridge Univ. (United Kingdom). Dept. of Engineering

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:9106.17(CUED/A-AERO/TR--23) / BLDSC ...

A source wake model for cascades of axial flow turbomachines

Ramirez Camacho, R. G.
Manzanares Filho, N.

September 2005

This work presents a computational model for the viscous flow through rectilinear cascades of axial ...

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...

Vortex boundary-layer interactions Semiannual status report

Bradshaw, P
Imperial Coll. of Science and Technology, London (United Kingdom). Dept. of Aeronautics

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:6015.42F(N--87-13666)(microfiche) / ...

Use of wakes to assist in the establishment of a turbulent boundary layer for proposed wind tunnel experiments with sprayers

Davis, P.F
AFRC Inst. of Engineering Research, Silsoe (United Kingdom). Sensors and Control Div

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3604.9221(AFRC-IER-DN--1400) / BLDSC...

Computational analysis of low speed axial flow rotors

Brown, K.D.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN015837 / BLDSC - British Library D...

Models for unsteady wake-induced transition in axial turbomachines

H. P. Hodson
J. S. Addison
C. A. Shepherson

January 1992

In turbomachinery, a considerable proportion of the blade surface area can be covered transitional b...

A study of unsteady wake-boundary layer interaction in turbomachines

Gete, Zenebe

January 1996

The relative motions of rotor and stator blade rows in a turbomachine generate periodically unstead...

Turbulence and complex flow phenomena in multi-stage axial turbomachines /

Katz, Joseph, author.
Meneveau, Charles, 1960-, author.
Johns Hopkins University, sponsor.
United States. Air Force. Office of Scientific Research, issuing body.

The objective of this project is to measure the flow within axial turbomachines and use the data to ...

Unsteady separated boundary layers in axial-flow turbomachinery

Schulte, V.

January 1995

SIGLEAvailable from British Library Document Supply Centre-DSC:D197438 / BLDSC - British Library Doc...

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

Walker, G.
Hughes, J.
Koehler, I.
Rolls-Royce plc (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92339) / BLDSC - British Lib...

Three-dimensional interaction of wakes and boundary layers

Moghadam, A.H.K

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:D59345 / BLDSC - British Library Doc...

A numerical study of the transonic blade-vortex interaction

Ng, N.L.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN027361 / BLDSC - British Library D...

An investigation into the unsteady blade interaction in one and a half stage axial flow turbine

Miller, R.J.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:D203928 / BLDSC - British Library Doc...

The interaction of a 2D turbulent wake with a bluff body

Ramsay, S.R

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:D60197 / BLDSC - British Library Doc...

Three-dimensional interaction of wake/boundary-layer and vortex/boundary-layer Data report

Yeung, C.
Squire, L
Cambridge Univ. (United Kingdom). Dept. of Engineering

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:9106.17(CUED/A-AERO/TR--23) / BLDSC ...

A source wake model for cascades of axial flow turbomachines

Ramirez Camacho, R. G.
Manzanares Filho, N.

September 2005

This work presents a computational model for the viscous flow through rectilinear cascades of axial ...

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...

Vortex boundary-layer interactions Semiannual status report

Bradshaw, P
Imperial Coll. of Science and Technology, London (United Kingdom). Dept. of Aeronautics

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:6015.42F(N--87-13666)(microfiche) / ...

Use of wakes to assist in the establishment of a turbulent boundary layer for proposed wind tunnel experiments with sprayers

Davis, P.F
AFRC Inst. of Engineering Research, Silsoe (United Kingdom). Sensors and Control Div

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3604.9221(AFRC-IER-DN--1400) / BLDSC...

Computational analysis of low speed axial flow rotors

Brown, K.D.

January 1998

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN015837 / BLDSC - British Library D...

Models for unsteady wake-induced transition in axial turbomachines

H. P. Hodson
J. S. Addison
C. A. Shepherson

January 1992

In turbomachinery, a considerable proportion of the blade surface area can be covered transitional b...

A study of unsteady wake-boundary layer interaction in turbomachines

Gete, Zenebe

January 1996

The relative motions of rotor and stator blade rows in a turbomachine generate periodically unstead...

Turbulence and complex flow phenomena in multi-stage axial turbomachines /

Katz, Joseph, author.
Meneveau, Charles, 1960-, author.
Johns Hopkins University, sponsor.
United States. Air Force. Office of Scientific Research, issuing body.

The objective of this project is to measure the flow within axial turbomachines and use the data to ...

Wake-boundary layer interaction in axial flow turbomachinery

Abstract

Extracted data

Wake-boundary layer interaction in axial flow turbomachinery

Abstract

Extracted data

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