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Simplified Numerical Models of the Unsteady Tip Leakage Flow in Compressor

SI Changxin WU Zihao LIU Xiaohua

热科学学报（英文版）2023，Vol.32Issue(6)：2386-2399,14.

热科学学报（英文版）2023，Vol.32Issue(6)：2386-2399,14.DOI:10.1007/S11630-023-1907-7

Simplified Numerical Models of the Unsteady Tip Leakage Flow in Compressor

SI Changxin ¹WU Zihao ²LIU Xiaohua³

作者信息

1. School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China
2. China Three Gorges Investment Management Co.,Ltd.,Shanghai 200124,China
3. School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China||Key Laboratory of Aerodynamic Noise Control,China Aerodynamics Research and Development Center,Mianyang 621000,China
折叠

摘要

关键词

turbomachinery/compressor/tip leakage flow/unsteady flow

Key words

turbomachinery/compressor/tip leakage flow/unsteady flow

引用本文复制引用

SI Changxin,WU Zihao,LIU Xiaohua..Simplified Numerical Models of the Unsteady Tip Leakage Flow in Compressor[J].热科学学报（英文版）,2023,32(6):2386-2399,14.

基金项目

This investigation is supported by the National Natural Science Foundation of China(No.51976116),National Science and Technology Major Project(No.j2019-ⅱ-0006-0026),and the Open Research Subject of Key Laboratory of Aerodynamic Noise Control(No.ANCL20230201). （No.51976116）

热科学学报（英文版）

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