Effects of Mach Number and Flow Incidence on Aerodynamic Losses of Steam Turbine Blades
An experiment was conducted to investigate the aerodynamic losses of two high-pressure steam turbine nozzles (526A, 525B) subjected to a large range of incident angle and exit Mach number. The blades were tested in a 2D transonic windtunnel. The exit Mach number ranged from 0.60 to 1.15 and the inci...
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Virginia Tech
2011
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| Online Access: | http://hdl.handle.net/10919/10093 http://scholar.lib.vt.edu/theses/available/etd-042399-112737 |