Experimental and Numerical Investigations of Optimized High-Turning Supercritical Compressor Blades
Cascade testing and flow analysis of three high-turning supercritical compressor blades were conducted. The blades were designed at an inlet Mach number (M1) of 0.87 and inlet flow angle of 48.4 deg, with high camber angles of about 55 deg. The baseline blade was a conventional Controlled Diffusion...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/29727 http://scholar.lib.vt.edu/theses/available/etd-11242003-025724/ |