Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole

Impingement channels are often used in turbine blade cooling configurations. This paper examines the heat transfer performance of a typical integrally cast impingement channel. Detailed heat transfer coefficient distributions on all heat transfer surfaces were obtained in a series of low temperature...

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主要な著者: Chambers, A, Gillespie, D, Ireland, P, Dailey, G
フォーマット: Journal article
言語:English
出版事項: American Society of Mechanical Engineers (ASME) 2003
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author Chambers, A
Gillespie, D
Ireland, P
Dailey, G
author_facet Chambers, A
Gillespie, D
Ireland, P
Dailey, G
author_sort Chambers, A
collection OXFORD
description Impingement channels are often used in turbine blade cooling configurations. This paper examines the heat transfer performance of a typical integrally cast impingement channel. Detailed heat transfer coefficient distributions on all heat transfer surfaces were obtained in a series of low temperature experiments carried out in a large-scale model of a turbine cooling system using liquid crystal techniques. All experiments were performed on a model of a 19-hole, low aspect ratio impingement channel. The effect of flow introduced at the inlet to the channel on the impingement heat transfer within the channel was investigated. A novel test technique has been applied to determine the effect of the initial cross flow on jet penetration. The experiments were performed at an engine representative Reynolds number of 20,000 and examined the effect of additional initial cross flow up to 10% of the total mass flow.
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spelling oxford-uuid:d9249aaa-6248-4749-9eaa-33ec4f30e9782022-03-27T08:53:46ZCooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first holeJournal articlehttp://purl.org/coar/resource_type/c_dcae04bcuuid:d9249aaa-6248-4749-9eaa-33ec4f30e978EnglishSymplectic Elements at OxfordAmerican Society of Mechanical Engineers (ASME)2003Chambers, AGillespie, DIreland, PDailey, GImpingement channels are often used in turbine blade cooling configurations. This paper examines the heat transfer performance of a typical integrally cast impingement channel. Detailed heat transfer coefficient distributions on all heat transfer surfaces were obtained in a series of low temperature experiments carried out in a large-scale model of a turbine cooling system using liquid crystal techniques. All experiments were performed on a model of a 19-hole, low aspect ratio impingement channel. The effect of flow introduced at the inlet to the channel on the impingement heat transfer within the channel was investigated. A novel test technique has been applied to determine the effect of the initial cross flow on jet penetration. The experiments were performed at an engine representative Reynolds number of 20,000 and examined the effect of additional initial cross flow up to 10% of the total mass flow.
spellingShingle Chambers, A
Gillespie, D
Ireland, P
Dailey, G
Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
title Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
title_full Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
title_fullStr Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
title_full_unstemmed Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
title_short Cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
title_sort cooling performance of a narrow impingement channel including the introduction of cross flow upstream of the first hole
work_keys_str_mv AT chambersa coolingperformanceofanarrowimpingementchannelincludingtheintroductionofcrossflowupstreamofthefirsthole
AT gillespied coolingperformanceofanarrowimpingementchannelincludingtheintroductionofcrossflowupstreamofthefirsthole
AT irelandp coolingperformanceofanarrowimpingementchannelincludingtheintroductionofcrossflowupstreamofthefirsthole
AT daileyg coolingperformanceofanarrowimpingementchannelincludingtheintroductionofcrossflowupstreamofthefirsthole