首页|期刊导航|中国航空学报（英文版）|Aerothermal performance of turbine during flight cycle based on fluid-thermal-structure multidisciplinary coupling method
Aerothermal performance of turbine during flight cycle based on fluid-thermal-structure multidisciplinary coupling methodOA
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
Research Institute of Aero-engine,Beihang University,Beijing 102206,ChinaResearch Institute of Aero-engine,Beihang University,Beijing 102206,ChinaResearch Institute of Aero-engine,Beihang University,Beijing 102206,ChinaResearch Institute of Aero-engine,Beihang University,Beijing 102206,ChinaAECC Sichuan Gas Turbine Establishment,Chengdu 610500,China
Flight cycleFluid-thermal-structureMultidisciplinary couplingQuasi-steady-stateTurbine
Flight cycleFluid-thermal-structureMultidisciplinary couplingQuasi-steady-stateTurbine
《中国航空学报（英文版）》 2026 (1)
35-54,20
This study was supported by the National Science and Tech-nology Major Project,China(No.J2019-Ⅱ-0012-0032),which is gratefully acknowledged.
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