Numerical prediction of the impact of non-uniform leading edge coatings on the aerodynamic performance of compressor airfoils
Approved for public release; distribution is unlimited === A computational fluid dynamic (CFD) investigation is presented that provides predictions of the aerodynamic impact of uniform and non-uniform coatings applied to the leading edge of a compressor airfoil in a cascade. Using a NACA 65(12)10 ai...
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/1158 |