Experimental investigation of cross-over jets in a rib-roughened trailing-edge cooling channel
Increasing the rotor inlet temperature can dramatically increase the efficiency and power output of the gas turbine engine. However, the melting point of turbine blade material limits the realistic upper bound of the rotor inlet temperature. As a result, the development of high temperature turbine b...
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| Online Access: | http://hdl.handle.net/2047/D20194325 |