An experimental study of heat transfer in the rectangular coolant passages of a gas turbine rotor blade /
Modern gas turbines have high inlet temperatures to harness maximum power output, which causes different components to experience severe thermal stresses and fatigue. To achieve turbine blade durability goals, the blades are cooled with air extracted from the compressor. The amount of air to be extr...
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| Format: | Thesis eBook |
| Language: | English |
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[Place of publication not identified] :
[publisher not identified] ;
2000.
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| Online Access: | Link to OAKTrust copy |
Internet
Link to OAKTrust copyCushing: Theses & Dissertations Microforms (Does not check out)
| Call Number: |
2000 Thesis U43 |
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| Call Number | Status | Get It |
| 2000 Thesis U43 | Available | |
Available Online
| Call Number: |
2000 Thesis U43 |
|
|---|---|---|
| Call Number | Status | Get It |
| 2000 Thesis U43 | Available | |