An investigation on turbine tip and shroud heat transfer
Detailed experimental investigations have been performed to measure the heat transfer and static pressure distributions on the rotor tip and rotor casing of a gas turbine stage with a shroud-less rotor blade. The turbine stage was a modern high pressure Rolls-Royce aero-engine design with stage pres...
| Main Authors: | , |
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| Format: | Journal article |
| Language: | English |
| Published: |
2002
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