Investigation of Turbine Stages with Radial Blades.

被引：0

作者：

Yakovlev, V.P.

Mityushkin, Yu.I.

机构：

来源：

Izvestiya Vysshikh Uchebnykh Zavedenij i Energeticheskikh Ob''edinenij Sng. Energetika | 1978年 / 04期

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摘要：

Results of aerodynamic investigations of turbine stages of medium D/l ratio with radial nozzle and rotor blades are presented. Two body thicknesses of nozzle blades are used in the investigations. The expediency of using turbine stages with radial nozzle and rotor blades as stages ensuring the required economic efficiency with a substantially lower gradient of the degree of reactivity over the height of the flow-through part is demonstrated.

引用

页码：57 / 61

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