Conference item
Detailed heat transfer measurements in a model of an integrally cast cooling passage
- Abstract:
-
Detailed measurements of the heat transfer coefficient distributions on the internal surfaces of a novel gas turbine blade cooling configuration were carried out using a transient liquid crystal technique. The cooling geometry, in which a series of racetrack passages are connected to a central plenum, provides high heat transfer coefficients in regions of the blade in good thermal contact with the outer blade surface. The Reynolds number changes along its length because of the ejection of flu...
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- Publication status:
- Published
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- Publisher copy:
- 10.1115/GT2006-91231
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Bibliographic Details
- Volume:
- 3 PART B
- Pages:
- 1015-1026
- Host title:
- Proceedings of the ASME Turbo Expo 2006, Vol 3, Pts A and B
- Publication date:
- 2006-01-01
- DOI:
- Source identifiers:
-
64564
- ISBN:
- 079184238X
Item Description
- Pubs id:
-
pubs:64564
- UUID:
-
uuid:5c99eae7-6813-4b4f-8c3c-c19eadb45f29
- Local pid:
- pubs:64564
- Deposit date:
- 2012-12-19
Terms of use
- Copyright date:
- 2006
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