Experimental investigation of turbine blade platform film cooling and rotational effect on trailing edge internal cooling
The present work has been an experimental investigation to evaluate the applicability of gas turbine cooling technology. With the temperature of the mainstream gas entering the turbine elevated above the melting temperature of the metal components, these components must be cooled, so they can withst...
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| Format: | Others |
| Language: | en_US |
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2010
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| Online Access: | http://hdl.handle.net/1969.1/ETD-TAMU-1826 http://hdl.handle.net/1969.1/ETD-TAMU-1826 |