Thermal control of gas turbine casings for improved tip clearance
<p>A thermal tip clearance control system provides a robust and flexible means of manipulating the closure between the casing and the rotating blade tips in a jet engine, reducing undesirable tip leakage flows. This may be achieved using an impingement cooling scheme on the external casing of...
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| Format: | Thesis |
| Language: | English |
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2015
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