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A Methodology for Assessing Axial Compressor Stability with Inlet Temperature Ramp Distortion

SUN Dakun GU Benhao NING Fangfei FANG Yibo DONG Xu XU Dengke SUN Xiaofeng

热科学学报(英文版)2024,Vol.33Issue(3):856-871,16.
热科学学报(英文版)2024,Vol.33Issue(3):856-871,16.DOI:10.1007/s11630-024-1961-9

A Methodology for Assessing Axial Compressor Stability with Inlet Temperature Ramp Distortion

A Methodology for Assessing Axial Compressor Stability with Inlet Temperature Ramp Distortion

SUN Dakun 1GU Benhao 1NING Fangfei 2FANG Yibo 1DONG Xu 2XU Dengke 1SUN Xiaofeng1

作者信息

  • 1. School of Energy and Power Engineering,Beihang University,Beijing 102206,China
  • 2. Research Institute of Aero-engine,Beihang University,Beijing 102206,China
  • 折叠

摘要

关键词

axial compressor stability/small perturbation model/inlet temperature ramp distortion/harmonic balance method/dynamic mode decomposition method

Key words

axial compressor stability/small perturbation model/inlet temperature ramp distortion/harmonic balance method/dynamic mode decomposition method

引用本文复制引用

SUN Dakun,GU Benhao,NING Fangfei,FANG Yibo,DONG Xu,XU Dengke,SUN Xiaofeng..A Methodology for Assessing Axial Compressor Stability with Inlet Temperature Ramp Distortion[J].热科学学报(英文版),2024,33(3):856-871,16.

基金项目

The research presented here is supported by National Natural Science Foundation of China(NSFC Grant Nos.52306036,52325602),Science Center for Gas Turbine Project(P2022-A-Ⅱ-002-001,P2022-C-Ⅱ-003-001),Project funded by China Postdoctoral Science Foundation(2022M720346)and National Science and Technology Major Project(Y2022-Ⅱ-0003-0006,Y2022-Ⅱ-0002-0005).Also,the research is supported by the Key Laboratory of Pre-Research Management Centre(No.6142702200101)and the Fundamental Research Funds for the Central Universities(YWF-23-Q-1009,YWF-23-Q-1065). (NSFC Grant Nos.52306036,52325602)

热科学学报(英文版)

OAEI

1003-2169

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