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郑赟 ( 副教授 ) 赞
的个人主页 http://shi.buaa.edu.cn/zhengyun/zh_CN/index.htm
副教授硕士生导师

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[1] .Optimization of the MSMGWB model used for the calculation of infrared remote sensing signals from hot combustion gases of hydrocarbon fuel.[期刊]:Infrared Physics & Technology,2020,107
[2] .A novel multi-fidelity coupled simulation method for flow systems, Chinese Journal of Aeronautics:Chinese Journal of Aeronautics,2013,21(4)
[3] .Coupled Fluid-structure Flutter Analysis of a Transonic Fan.[期刊]:Chinese Journal of Aeronautics,2011,24(3)
[4] .Aeroelastic vibration analysis of a 1.5 stage compressor:Propulsion and Power Research,2019,1(9)
[5] .Non-synchronous blade vibration analysis of a transonic fan.[期刊]:Chinese Journal of Aeronautics,1(36):178-190
[6] .Effects of Asymmetric Vane Pitch on Reducing Low-Engine-Order Forced Response of a Turbine Stage.[期刊]:Aerospace,2022,11(9)
[7] .A Modified Shielding and Rapid Transition DDES Model for Separated Flows:Entropy,2022,1(25)
[8] .Forced Response Analysis of an Embedded Compressor Rotor Induced by Stator Disturbances and Rotor–Stator Interactions.[期刊]:Aerospace,2023,1(10)
[9] .Low-Engine-Order Forced Response Analysis of a Turbine Stage with Damaged Stator Vane.[期刊]:Entropy,4(26)
[10] .Effect of Intake Acoustic Reflection on Blade Vibration Characteristics.[期刊]:Aerospace,2024,5(11)

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