Experimental Study of the Flow Field in a Model 1.5-Stage Gas Turbine Rotor-Stator Disk Cavity
abstract: A major concern in the operation of present-day gas turbine engines is the ingestion of hot mainstream gas into rotor-stator disk cavities of the high-pressure turbine stages. Although the engines require high gas temperature at turbine entry for good performance efficiency, the ingested g...
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| Format: | Dissertation |
| Language: | English |
| Published: |
2010
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| Online Access: | http://hdl.handle.net/2286/R.I.8719 |