Analysis of leakage flow and loss in a linear compressor cascade with moving endwall-Reference-Cited by-同舟云学术

Analysis of leakage flow and loss in a linear compressor cascade with moving endwall

Published:2022-11-10 Issue:1 Volume:6 Page:107-118
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Deng Hefang^ORCID,Xia Kailong,Teng Jinfang,Qiang Xiaoqing,Zhu Mingmin,Lu Shaopeng

Funder

the Natural Science Foundation of China

the National Science and Technology Major Project

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-022-00173-7.pdf

Reference21 articles.

1. Evans S, Yi J, Nolan S et al (2021) Modeling of axial compressor with large tip clearances. J Turbomach 143(6):061007

2. Denton JD (1993) Loss mechanisms in turbomachines. ASME Paper GT1993-435

3. Wisler DC (1985) Loss reduction in axial-flow compressors through low-speed model testing. J Eng Gas Turbines Power 107(2):354–363

4. Sakulkaew S, Tan CS, Donahoo E et al (2013) Compressor efficiency variation with rotor tip gap from vanishing to large clearance. J Turbomach 135(3):031030

5. Williams R, Gregory-Smith D, He L et al (2010) Experiments and computations on large tip clearance effects in a linear cascade. J Turbomach 132(2):021018

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1. Effects of moving endwall on the unsteadiness of tip leakage flow in compressor cascades;Physics of Fluids;2023-08-01