EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING

The benefits of different film cooling geometries are typically assessed in terms of their time-averaged performance. It is known that the mixing between the coolant film and the main turbine passage flow is an unsteady process. The current study investigates the forms of unsteadiness that occur in...

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Main Authors: Fawcett, R, Wheeler, A, He, L, Taylor, R, ASME
Format: Conference item
Published: 2010
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author Fawcett, R
Wheeler, A
He, L
Taylor, R
ASME
author_facet Fawcett, R
Wheeler, A
He, L
Taylor, R
ASME
author_sort Fawcett, R
collection OXFORD
description The benefits of different film cooling geometries are typically assessed in terms of their time-averaged performance. It is known that the mixing between the coolant film and the main turbine passage flow is an unsteady process. The current study investigates the forms of unsteadiness that occur in engine-representative film cooling flows and how this unsteadiness affects the mixing with the mainstream flow. Cylindrical and fan-shaped cooling holes across a range of hole blowing ratios have been studied experimentally using particle image velocimetry and high speed photography. Coherent unsteadiness is found in the shear layer between the jet and the mainstream for both cylindrical and fan-shaped cooling holes. Its occurrence and sense of rotation is found to be controlled by the velocity difference between the mainstream flow and the jet, which is largely determined by the blowing ratio. © 2012 American Society of Mechanical Engineers.
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spelling oxford-uuid:878ed853-e655-49dd-a890-a854d40140e82022-03-26T22:11:28ZEXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLINGConference itemhttp://purl.org/coar/resource_type/c_5794uuid:878ed853-e655-49dd-a890-a854d40140e8Symplectic Elements at Oxford2010Fawcett, RWheeler, AHe, LTaylor, RASMEThe benefits of different film cooling geometries are typically assessed in terms of their time-averaged performance. It is known that the mixing between the coolant film and the main turbine passage flow is an unsteady process. The current study investigates the forms of unsteadiness that occur in engine-representative film cooling flows and how this unsteadiness affects the mixing with the mainstream flow. Cylindrical and fan-shaped cooling holes across a range of hole blowing ratios have been studied experimentally using particle image velocimetry and high speed photography. Coherent unsteadiness is found in the shear layer between the jet and the mainstream for both cylindrical and fan-shaped cooling holes. Its occurrence and sense of rotation is found to be controlled by the velocity difference between the mainstream flow and the jet, which is largely determined by the blowing ratio. © 2012 American Society of Mechanical Engineers.
spellingShingle Fawcett, R
Wheeler, A
He, L
Taylor, R
ASME
EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING
title EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING
title_full EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING
title_fullStr EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING
title_full_unstemmed EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING
title_short EXPERIMENTAL INVESTIGATION INTO UNSTEADY EFFECTS ON FILM COOLING
title_sort experimental investigation into unsteady effects on film cooling
work_keys_str_mv AT fawcettr experimentalinvestigationintounsteadyeffectsonfilmcooling
AT wheelera experimentalinvestigationintounsteadyeffectsonfilmcooling
AT hel experimentalinvestigationintounsteadyeffectsonfilmcooling
AT taylorr experimentalinvestigationintounsteadyeffectsonfilmcooling
AT asme experimentalinvestigationintounsteadyeffectsonfilmcooling