Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade
Large tip clearances typically in the region of 6% exist in the high pressure (HP) 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...
| Main Authors: | , , , |
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| 格式: | Conference item |
| 出版: |
2010
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