Conjugate Heat Transfer of an Internally Air-Cooled Nozzle Guide Vane and Shrouds
نویسندگان
چکیده
منابع مشابه
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 by a complex vortical secondary flow at the junction of the endwall and the airfoil. This flow t...
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ژورنال
عنوان ژورنال: Advances in Mechanical Engineering
سال: 2014
ISSN: 1687-8140,1687-8140
DOI: 10.1155/2014/146523