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Efficient methods for prediction and evaluation of compressor rotor blades forced response considering multiple excitation from asymmetric stators

Yuze ZHU Ping YANG Jinzhang FENG Dingxi WANG Zhuo KOU

中国航空学报（英文版）2026，Vol.39Issue(3)：294-308,15.

中国航空学报（英文版）2026，Vol.39Issue(3)：294-308,15.DOI:10.1016/j.cja.2025.103805

Efficient methods for prediction and evaluation of compressor rotor blades forced response considering multiple excitation from asymmetric stators

Yuze ZHU ¹Ping YANG ²Jinzhang FENG ³Dingxi WANG ⁴Zhuo KOU²

作者信息

1. AECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,China||National Elite Institute of Engineering,Northwestern Polytechnical University,Xi'an 710072,China
2. AECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,China
3. AECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,China||School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China
4. School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China
折叠

摘要

关键词

Asymmetric stators/Nonuniform pitches/Forced response/Fourier-based method/Multiple excitation compo-nents/Time inclination method

Key words

Asymmetric stators/Nonuniform pitches/Forced response/Fourier-based method/Multiple excitation compo-nents/Time inclination method

引用本文复制引用

Yuze ZHU,Ping YANG,Jinzhang FENG,Dingxi WANG,Zhuo KOU..Efficient methods for prediction and evaluation of compressor rotor blades forced response considering multiple excitation from asymmetric stators[J].中国航空学报（英文版）,2026,39(3):294-308,15.

基金项目

The authors would like to express their sincere gratitude to Distinguished Researcher Huang HUANG from Tianmushan Laboratory for his valuable support and assistance throughout this work.This work was also supported by the Aeronautical Science Foundation of China(Nos.2023L039053002 and 2024M039053001). （Nos.2023L039053002 and 2024M039053001）

中国航空学报（英文版）

ISSN：1000-9361

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