experimental investigation of impingement cooling in an airfoil leading-edge cavity
An experimental investigation was carried out to determine the effects of the number of unblocked cross-over holes and different flow arrangements on heat transfer coefficients in impingement cooling over a curved surface, simulating the leading-edge cooling cavity of an airfoil. A jet plate through...
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| Online Access: | http://hdl.handle.net/2047/d20000792 |