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Simulating inlet total temperature distortion flows in transonic compressor based on time-space collocation method

Lei WU Pengcheng DU Fangfei NING

中国航空学报(英文版)2026,Vol.39Issue(6):125-142,18.
中国航空学报(英文版)2026,Vol.39Issue(6):125-142,18.DOI:10.1016/j.cja.2025.104002

Simulating inlet total temperature distortion flows in transonic compressor based on time-space collocation method

Simulating inlet total temperature distortion flows in transonic compressor based on time-space collocation method

Lei WU 1Pengcheng DU 1Fangfei NING1

作者信息

  • 1. Research Institute of Aero-Engine,Beihang University,Beijing 102206,China||National Key Laboratory of Science and Technology on Aero-Engines,Beihang University,Beijing 102206,China
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摘要

关键词

Inlet total temperature dis-tortion/Temporal harmonics/Time-space collocation method/Spatial harmonics/Unsteady flows

Key words

Inlet total temperature dis-tortion/Temporal harmonics/Time-space collocation method/Spatial harmonics/Unsteady flows

引用本文复制引用

Lei WU,Pengcheng DU,Fangfei NING..Simulating inlet total temperature distortion flows in transonic compressor based on time-space collocation method[J].中国航空学报(英文版),2026,39(6):125-142,18.

中国航空学报(英文版)

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