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Aerothermal performance of turbine during flight cycle based on fluid-thermal-structure multidisciplinary coupling method

Yunda ZHANG Zhengping ZOU Chao FU Yifan WANG Jun ZENG

中国航空学报（英文版）2026，Vol.39Issue(1)：35-54,20.

中国航空学报（英文版）2026，Vol.39Issue(1)：35-54,20.DOI:10.1016/j.cja.2025.103691

Aerothermal performance of turbine during flight cycle based on fluid-thermal-structure multidisciplinary coupling method

Yunda ZHANG ¹Zhengping ZOU ¹Chao FU ¹Yifan WANG ¹Jun ZENG²

作者信息

1. Research Institute of Aero-engine,Beihang University,Beijing 102206,China
2. AECC Sichuan Gas Turbine Establishment,Chengdu 610500,China
折叠

摘要

关键词

Flight cycle/Fluid-thermal-structure/Multidisciplinary coupling/Quasi-steady-state/Turbine

Key words

Flight cycle/Fluid-thermal-structure/Multidisciplinary coupling/Quasi-steady-state/Turbine

引用本文复制引用

Yunda ZHANG,Zhengping ZOU,Chao FU,Yifan WANG,Jun ZENG..Aerothermal performance of turbine during flight cycle based on fluid-thermal-structure multidisciplinary coupling method[J].中国航空学报（英文版）,2026,39(1):35-54,20.

基金项目

This study was supported by the National Science and Tech-nology Major Project,China(No.J2019-Ⅱ-0012-0032),which is gratefully acknowledged. （No.J2019-Ⅱ-0012-0032）

中国航空学报（英文版）

ISSN：1000-9361

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