Gas turbine engine turbine blade tip cooling
作者： James T. Auxier , Jason L. O'hearn , Thomas N. Slavens , Yafet Girma
DOI:
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摘要: An airfoil for a gas turbine engine includes pressure and suction walls spaced apart from one another joined at leading trailing edges to provide an having exterior surface that extends in radial direction tip. A camber line the tip edge edge. Pressure side shelves are arranged on opposing sides of respectively walls. plateau is proud separates shelves. The along
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