Numerical prediction of flow and heat transfer in the coolant passages of a gas turbine rotor blade /
Numerical prediction of three- dimensional flow and heat transfer was performed for four cases. 1) A rotating/non-rotating smooth square channel with 180⁰ bend in which the rotation number was varied from 0 to 0.24, the inlet coolant-to-wall density ratio was varied from 0 to 0.22, while the Reynold...
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| Format: | Thesis Book |
| Language: | English |
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[Place of publication not identified] :
[publisher not identified] ;
2000.
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| Call Number: |
2000 Dissertation J35 |
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| Call Number | Status | Get It |
| 2000 Dissertation J35 | Available | |
Available Online
| Call Number: |
2000 Dissertation J35 |
|
|---|---|---|
| Call Number | Status | Get It |
| 2000 Dissertation J35 | Available | |