Steady and Unsteady Heat Transfer in a Film Cooled Transonic Turbine Cascade
The unsteady interaction of shock waves emerging from the trailing edge of modern turbine nozzle guide vanes and impinging on downstream rotor blades is modeled in a linear cascade. The Reynolds number based on blade chord and exit conditions (5*10^6) and the exit Mach number (1.2) are representativ...
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| Format: | Others |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/28513 http://scholar.lib.vt.edu/theses/available/etd-080399-154049/ |