Optimization and experimental study of stationary endwall of stator labyrinth cavity in a low-speed research compressor-Reference-Cited by-同舟云学术

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Optimization and experimental study of stationary endwall of stator labyrinth cavity in a low-speed research compressor

Published:2024-04 Issue: Volume:147 Page:109036
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zheng Biaojie^ORCID,Shao Runzhu^ORCID,Zhang Songan,Zhu Mingmin,Qiang Xiaoqing,Teng Jinfang^ORCID

Funder

NSFC

Publisher

Elsevier BV

Reference34 articles.

1. Loss analysis of cavity leakage flow in a compressor cascade;Deng;J. Turbomach.,2022

2. The influence of shrouded stator cavity flows on multistage compressor performance;Wellborn;J. Turbomach.,1999

3. Details of shrouded stator hub cavity flow in a multistage axial compressor part 2: leakage flow characteristics in stator wells;Kamdar;J. Eng. Gas Turbine Power,2022

4. Influence of seal cavity leakage flow on compressor performance investigated with a circumferentially averaged method;Liang;Appl. Sci.,2021

5. Different effects of cantilevered and shrouded stators on axial compressor performance;Si,2017

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Adjoint-Based Finely Integrated Design of Endwall Region for a Linear Cascade;2024

2. Research on Several Approaches for Integrated Passage Design of Compressor;2024

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