Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes
Trailing edge cooling cavities in modern gas turbine airfoils play an important role in maintaining the trailing edge temperature at levels consistent with airfoil design life. These cavities often have a trapezoidal cross-sectional shape in order to be compatible with the external contour of the bl...
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| Online Access: | http://hdl.handle.net/2047/d20000061 |