Aerodynamic optimization of a heavy-duty gas turbine vane: Synergizing non-axisymmetric endwall contouring with 3D blade profiling

已完结 10 由轩诺发布于 2026/10/16 11:14:03

DOI:10.1016/j.ast.2026.112749
作者：Peng Qin ,?Zhengshuai Du ,?Yingjie Chen ,?Le Cai ,?Songtao Wang
文献类型：期刊论文
补充材料：只需要正文

Elsevier

Abstract：To address the complex flow characteristics within the first-stage vane passage of a high-load heavy-duty gas turbine under transonic conditions (with an exit Mach number of 0.9), this study

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