Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets

Full heat transfer coefficient and static pressure distributions have been measured on the target surface under impinging jets formed by sharp-edged and large entry radius holes. These geometries are representative of impingement holes in a gas turbine blade manufactured by laser cutting and by cast...

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Main Authors: Gillespie, D, Guo, S, Wang, Z, Ireland, P, Kohler, S
Format: Journal article
Language:English
Published: ASME 1996
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author Gillespie, D
Guo, S
Wang, Z
Ireland, P
Kohler, S
author_facet Gillespie, D
Guo, S
Wang, Z
Ireland, P
Kohler, S
author_sort Gillespie, D
collection OXFORD
description Full heat transfer coefficient and static pressure distributions have been measured on the target surface under impinging jets formed by sharp-edged and large entry radius holes. These geometries are representative of impingement holes in a gas turbine blade manufactured by laser cutting and by casting, respectively. Target surface heat transfer has been measured in a large scale perspex rig using both the transient liquid crystal technique and hot thin film gauges. A range of jet Reynolds numbers, representative of engine conditions, has been investigated. The velocity variation has been calculated from static pressure measurements on the impingement target surface. The heat transfer to the target surface is discussed in terms of the interpreted flow field.
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spelling oxford-uuid:9ae9e90f-76a2-428a-a55a-7d309fc586442022-03-27T00:24:45ZComparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jetsJournal articlehttp://purl.org/coar/resource_type/c_dcae04bcuuid:9ae9e90f-76a2-428a-a55a-7d309fc58644EnglishSymplectic Elements at OxfordASME1996Gillespie, DGuo, SWang, ZIreland, PKohler, SFull heat transfer coefficient and static pressure distributions have been measured on the target surface under impinging jets formed by sharp-edged and large entry radius holes. These geometries are representative of impingement holes in a gas turbine blade manufactured by laser cutting and by casting, respectively. Target surface heat transfer has been measured in a large scale perspex rig using both the transient liquid crystal technique and hot thin film gauges. A range of jet Reynolds numbers, representative of engine conditions, has been investigated. The velocity variation has been calculated from static pressure measurements on the impingement target surface. The heat transfer to the target surface is discussed in terms of the interpreted flow field.
spellingShingle Gillespie, D
Guo, S
Wang, Z
Ireland, P
Kohler, S
Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
title Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
title_full Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
title_fullStr Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
title_full_unstemmed Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
title_short Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
title_sort comparison of full surface local heat transfer coefficient and flow field studies beneath sharp edged and radiused entry impinging jets
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AT wangz comparisonoffullsurfacelocalheattransfercoefficientandflowfieldstudiesbeneathsharpedgedandradiusedentryimpingingjets
AT irelandp comparisonoffullsurfacelocalheattransfercoefficientandflowfieldstudiesbeneathsharpedgedandradiusedentryimpingingjets
AT kohlers comparisonoffullsurfacelocalheattransfercoefficientandflowfieldstudiesbeneathsharpedgedandradiusedentryimpingingjets