Aerodynamic performance of a transonic turbine blade passage in presence of upstream slot and mateface gap with endwall contouring
The present study investigates mixed out aerodynamic loss coefficient measurements for a high turning, contoured endwall passage under transonic operating conditions in presence of upstream purge slot and mateface gap. The upstream purge slot represents the gap between stator-rotor interface and the...
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| Format: | Others |
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Virginia Tech
2015
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| Online Access: | http://hdl.handle.net/10919/54577 |