On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition Duct

被引：0
作者：
Remizov A.E. [1 ]
Vyatkov V.V. [1 ]
Lebedev V.V. [1 ]
机构：
[1] Rybinsk State Aviation Technical University, ul. Pushkina 53, Rybinsk
来源：
Russian Aeronautics | 2017年 / 60卷 / 04期
关键词：
annular diffuser; flow swirl; loss ratio; turbine spool;
D O I：
10.3103/S1068799817040195
中图分类号：
学科分类号：
摘要：
The paper highlights significance of the interturbine transition duct as part of the high pressure and low pressure turbine spool. The correlations have been suggested allowing us to estimate variation of the average cross section flow swirl while its passing the interturbine transition duct. © 2017, Allerton Press, Inc.
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收藏
页码：616 / 620
页数：4
相关论文
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