Measurement and analysis of gas turbine blade tip heat transfer and film cooling /
The continuing trend toward high gas turbine inlet temperature has resulted in a high heat load on turbine components. The blade tip is one of the most critical regions because of the high heat load and difficulty in cooling. Therefore, the detailed information of heat transfer coefficient and film...
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| Format: | Thesis Book |
| Language: | English |
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[Place of publication not identified] :
[publisher not identified] ;
2002.
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| Call Number: |
2002 Dissertation K86 |
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| Call Number | Status | Get It |
| 2002 Dissertation K86 | Available | |
Available Online
| Call Number: |
2002 Dissertation K86 |
|
|---|---|---|
| Call Number | Status | Get It |
| 2002 Dissertation K86 | Available | |