Heat transfer, adiabatic effectiveness and injectant distributions downstream of single and double rows of film-cooling holes with compound angles
Approved for public release; distribution unlimited. === Experimental results are presented which describe the development and structure of turbulent boundary layer flow downstream of single and double rows of film-cooling holes with compound angles. The film-cooling holes are inclined at an angle o...
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Monterey, California: Naval Postgraduate School
2013
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| Online Access: | http://hdl.handle.net/10945/34872 |