Numerical Solution of a Direct Problem of Calculation of the Three-dimensional Transonic Flow in a Turbine Stage.

被引:0
作者
Gnesin, V.I.
机构
来源
Teploenergetika | 1982年 / 11期
关键词
TURBOMACHINERY;
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摘要
A numerical method of calculation of the three-dimensional flow of turbomachinery gas in an axial turbomachinery stage is proposed. It takes account of the aerodynamic interaction between the stator and the rotor. Results of a computational investigation of a spatial transonic flow in the last stage of a high-capacity steam turbine are presented.
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页码:35 / 39
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