Numerical Simulation on Unsteady Flow Mechanism of a 1.5-Stage Axial Transonic CompressorOAEI
In this paper,a numerical simulation method is used to calculate a 1.5-stage axial transonic compressor to explore its unsteady flow mechanism.The performance curve is compared with the experimental data to verify the calcula…查看全部>>
PENG Shuxuan;ZHANG Xiaoyu;WANG Wentao;ZHANG Hongwu;LI Xinlong
High Efficiency and Low Carbon Gas Turbine Digitalization Research Centre,Nanjing Institute of Future Energy System,Nanjing 211135,ChinaAdvanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China Key Laboratory of Advanced Energy and Power,Chinese Academy of Sciences,Beijing 100190,China Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,China University of Chinese Academy of Sciences,Beijing 100049,ChinaAdvanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China Key Laboratory of Advanced Energy and Power,Chinese Academy of Sciences,Beijing 100190,China Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,ChinaHigh Efficiency and Low Carbon Gas Turbine Digitalization Research Centre,Nanjing Institute of Future Energy System,Nanjing 211135,China Advanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China Key Laboratory of Advanced Energy and Power,Chinese Academy of Sciences,Beijing 100190,China Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,China University of Chinese Academy of Sciences,Beijing 100049,ChinaBYD Auto Industry Company Limited,Shenzhen 518116,China
能源与动力
numerical simulationaxial transonic compressorunsteady flowvortex breakdown
《Journal of Thermal Science》 2024 (5)
P.1851-1866,16
the support of the grants of Strategic Priority Research Program of the Chinese Academy of Sciences(No.XDA29050500)。
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