Heat transfer from low aspect ratio pin fins

Michael E. Lyall, Alan A. Thrift, Atul Kohli, Karen A. Thole

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Scopus citations

Abstract

The performance of many engineering devices from power electronics to gas turbines is limited by thermal management. Heat transfer augmentation in internal flows is commonly achieved through the use of pin fins, which increase both surface area and turbulence. The present research is focused on internal cooling of turbine airfoils using a single row of circular pin fins that is oriented perpendicular to the flow. Low aspect ratio pin fins were studied whereby the channel height to pin diameter was unity. A number of spanwise spacings were investigated for a Reynolds number range between 5000 to 30,000. Both pressure drop and spatially-resolved heat transfer measurements were taken. The heat transfer measurements were made on the endwall of the pin fin array using infrared thermography and on the pin surface using discrete thermocouples. The results show that the heat transfer augmentation relative to open channel flow is the highest for smallest spanwise spacings and lowest Reynolds numbers. The results also indicate that the pin fin heat transfer is higher than the endwall heat transfer.

Original languageEnglish (US)
Title of host publicationProceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air
Pages413-422
Number of pages10
DOIs
StatePublished - Sep 24 2007
Event2007 ASME Turbo Expo - Montreal, Que., Canada
Duration: May 14 2007May 17 2007

Publication series

NameProceedings of the ASME Turbo Expo
Volume4 PART A

Other

Other2007 ASME Turbo Expo
CountryCanada
CityMontreal, Que.
Period5/14/075/17/07

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All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Lyall, M. E., Thrift, A. A., Kohli, A., & Thole, K. A. (2007). Heat transfer from low aspect ratio pin fins. In Proceedings of the ASME Turbo Expo 2007 - Power for Land, Sea, and Air (pp. 413-422). (Proceedings of the ASME Turbo Expo; Vol. 4 PART A). https://doi.org/10.1115/GT2007-27431