Experimental heat transfer in midchord and leading edge turbine blade cooling passages with staggered turbulators
Modern gas turbine engines use various methods of convective cooling to protect hot section components from wear and to permit the engine to operate at higher turbine inlet temperatures for increased efficiency. One method of cooling is through internal passages roughened with turbulators to enhance...
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| Online Access: | http://hdl.handle.net/2047/d20005036 |