Heat transfer in leading and trailing edge cooling channels of the gas turbine blade under high rotation numbers
The gas turbine blade/vane internal cooling is achieved by circulating the compressed air through the cooling passages inside the turbine blade. Leading edge and trailing edge of the turbine blade are two critical regions which need to be properly cooled. Leading edge region receives extremely hot m...
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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-3196 http://hdl.handle.net/1969.1/ETD-TAMU-3196 |