Endwall Heat Transfer and Shear Stress for a Nozzle Guide Vane with Fillets and a Leakage Interface
Increasing the combustion temperatures in a gas turbine engine to achieve higher efficiency and power output also results in high heat loads to turbine components downstream of the combustor. The challenge of adequately cooling the nozzle guide vane directly downstream of the combustor is compounded...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/31912 http://scholar.lib.vt.edu/theses/available/etd-04252007-092722/ |