EXPERIMENTS AND COMPUTATIONS ON LARGE TIP CLEARANCE EFFECTS IN A LINEAR CASCADE

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 increa...

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Bibliografske podrobnosti
Main Authors:	Williams, R, Gregory-Smith, D, He, L, Ingram, G, ASME
Format:	Conference item
Izdano:	2008

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade od Williams, R, Gregory-Smith, D, He, L, Ingram, G

Izdano 2010

Conference item

EXPERIMENTS AND COMPUTATIONS ON LARGE TIP CLEARANCE EFFECTS IN A LINEAR CASCADE

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade od Williams, R, Gregory-Smith, D, He, L, Ingram, G

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