Turbine blade tip aero-thermal management: Some recent advances and research outlook

This article provides an overview of some recent progress in understanding HP turbine blade shroudless tip heat transfer and aerodynamics, especially in a transonic regime. The review is mostly based on the experimental and numerical efforts the authors have been involved in during the past ten year...

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Main Authors: Zhang, Q, He, L
Format: Journal article
Published: Global Power and Propulsion Society 2017
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author Zhang, Q
He, L
author_facet Zhang, Q
He, L
author_sort Zhang, Q
collection OXFORD
description This article provides an overview of some recent progress in understanding HP turbine blade shroudless tip heat transfer and aerodynamics, especially in a transonic regime. The review is mostly based on the experimental and numerical efforts the authors have been involved in during the past ten years. Some fundamental flow physics especially in high speed Over-TipLeakage (OTL) flows are highlighted, including tip choking, shock waves, and the roles played by flow turbulence, etc. These mechanisms bring qualitative differences in tip heat transfer and loss generation, and prospects in tip aerothermal management and control. Of great interest is the strong OTL flow–coolant interaction, which can dramatically affect the tip aerodynamics, and thus would challenge any “optimized” tip geometry based on an uncooled configuration. It is suggested that optimal tip aero-thermal configurations should be an iterative process between blade tip shaping and cooling injection scheme. Combining tip geometry shaping and cooling injection patterns concurrently may provide more extensive exploitation of tip aerothermal design space.
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spelling oxford-uuid:c157277d-11db-4ec1-bad2-34657cf6d1252022-03-27T06:00:47ZTurbine blade tip aero-thermal management: Some recent advances and research outlookJournal articlehttp://purl.org/coar/resource_type/c_dcae04bcuuid:c157277d-11db-4ec1-bad2-34657cf6d125Symplectic Elements at OxfordGlobal Power and Propulsion Society2017Zhang, QHe, LThis article provides an overview of some recent progress in understanding HP turbine blade shroudless tip heat transfer and aerodynamics, especially in a transonic regime. The review is mostly based on the experimental and numerical efforts the authors have been involved in during the past ten years. Some fundamental flow physics especially in high speed Over-TipLeakage (OTL) flows are highlighted, including tip choking, shock waves, and the roles played by flow turbulence, etc. These mechanisms bring qualitative differences in tip heat transfer and loss generation, and prospects in tip aerothermal management and control. Of great interest is the strong OTL flow–coolant interaction, which can dramatically affect the tip aerodynamics, and thus would challenge any “optimized” tip geometry based on an uncooled configuration. It is suggested that optimal tip aero-thermal configurations should be an iterative process between blade tip shaping and cooling injection scheme. Combining tip geometry shaping and cooling injection patterns concurrently may provide more extensive exploitation of tip aerothermal design space.
spellingShingle Zhang, Q
He, L
Turbine blade tip aero-thermal management: Some recent advances and research outlook
title Turbine blade tip aero-thermal management: Some recent advances and research outlook
title_full Turbine blade tip aero-thermal management: Some recent advances and research outlook
title_fullStr Turbine blade tip aero-thermal management: Some recent advances and research outlook
title_full_unstemmed Turbine blade tip aero-thermal management: Some recent advances and research outlook
title_short Turbine blade tip aero-thermal management: Some recent advances and research outlook
title_sort turbine blade tip aero thermal management some recent advances and research outlook
work_keys_str_mv AT zhangq turbinebladetipaerothermalmanagementsomerecentadvancesandresearchoutlook
AT hel turbinebladetipaerothermalmanagementsomerecentadvancesandresearchoutlook