Efficient methods for prediction and evaluation of compressor rotor blades forced response considering multiple excitation from asymmetric statorsOA
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
AECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,China||National Elite Institute of Engineering,Northwestern Polytechnical University,Xi'an 710072,ChinaAECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,ChinaAECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,China||School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,ChinaSchool of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,ChinaAECC Commercial Aircraft Engine Co.,Ltd,Shanghai 200241,China
Asymmetric statorsNonuniform pitchesForced responseFourier-based methodMultiple excitation compo-nentsTime inclination method
Asymmetric statorsNonuniform pitchesForced responseFourier-based methodMultiple excitation compo-nentsTime inclination method
《中国航空学报（英文版）》 2026 (3)
294-308,15
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).
评论