Conference item
EXPERIMENTS AND COMPUTATIONS ON LARGE TIP CLEARANCE EFFECTS IN A LINEAR CASCADE
- Abstract:
-
Large tip clearances typically in the region of six percent exist in the high pressure stages of compressors of industrial gas turbines. Due to the relatively short annulus height and significant blockage, the tip clearance flow accounts for the largest proportion of loss in the HP. Therefore increasing the understanding of such flows will allow for improvements in design of such compressors, increasing efficiency, stability and the operating range. Experimental and computational techniques h...
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- Publication status:
- Published
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Bibliographic Details
- Host title:
- PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A
- Volume:
- 6
- Issue:
- PART A
- Pages:
- 335-347
- Publication date:
- 2008-01-01
- DOI:
- ISBN:
- 9780791843161
Item Description
- Pubs id:
-
pubs:62106
- UUID:
-
uuid:e1370d4c-a202-4056-aac5-222777abb5ef
- Local pid:
-
pubs:62106
- Source identifiers:
-
62106
- Deposit date:
-
2013-11-16
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- Copyright date:
- 2008
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