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Computational Study of the Effects of Shroud Geometric Variation on Turbine Performance in a 1.5-Stage High-Loaded Turbine

Wei Jia Huoxing Liu

热科学学报（英文版）2013，Vol.22Issue(5)：439-446,8.

热科学学报（英文版）2013，Vol.22Issue(5)：439-446,8.DOI:10.1007/s11630-013-0646-6

Computational Study of the Effects of Shroud Geometric Variation on Turbine Performance in a 1.5-Stage High-Loaded Turbine

Wei Jia ¹Huoxing Liu¹

作者信息

1. National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing 100191, China
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摘要

关键词

labyrinth seal/tip shroud geometry/shroud leakage flow/turbine performance/high-loaded turbine

Key words

labyrinth seal/tip shroud geometry/shroud leakage flow/turbine performance/high-loaded turbine

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Wei Jia,Huoxing Liu..Computational Study of the Effects of Shroud Geometric Variation on Turbine Performance in a 1.5-Stage High-Loaded Turbine[J].热科学学报（英文版）,2013,22(5):439-446,8.

基金项目

Financial support from the Innovation Foundation of BUAA for PhD Graduates (YWF-13-A01-014) （YWF-13-A01-014）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

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