Improvement of Gas-Dynamic Efficiency of GTE Gas Turbine Stages at the Design Stage

A. E. Remizov; V. V. Vyatkov; V. A. Lebedev

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Improvement of Gas-Dynamic Efficiency of GTE Gas Turbine Stages at the Design Stage

机译：设计阶段GTE燃气轮机级燃气动力效率的提高

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摘要

Methods to control flow have been considered in order to reduce end losses in blade rows of GTE gas turbines by means of measures taken at the design stage.

机译：为了通过在设计阶段采取的措施来减少GTE燃气轮机叶片排的端部损耗，已经考虑了控制流量的方法。

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来源
《Russian Aeronautics》 |2016年第4期|559-564|共6页
作者
A. E. Remizov; V. V. Vyatkov; V. A. Lebedev;
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作者单位

Rybinsk State Aviation Technical University;

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原文格式 PDF
正文语种英语
中图分类航空;
关键词
Loading parameter; Blade height; Radial clearance; Secondary flows; Loss coefficient; Flow control; Optimization;

机译：加载参数;刀片高度;径向间隙;二次流;损耗系数;流量控制;优化;

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Improvement of Gas-Dynamic Efficiency of GTE Gas Turbine Stages at the Design Stage

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