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Yun ZHENG

Personal Information

Associate Professor
Supervisor of Master's Candidates

Paper

.Optimization of the MSMGWB model used for the calculation of infrared remote sensing signals from hot combustion gases of hydrocarbon fuel.[J]:Infrared Physics & Technology,2020,107
.A novel multi-fidelity coupled simulation method for flow systems, Chinese Journal of Aeronautics:Chinese Journal of Aeronautics,2013,21(4)
.Coupled Fluid-structure Flutter Analysis of a Transonic Fan.[J]:Chinese Journal of Aeronautics,2011,24(3)
.Aeroelastic vibration analysis of a 1.5 stage compressor:Propulsion and Power Research,2019,1(9)
.Non-synchronous blade vibration analysis of a transonic fan.[J]:Chinese Journal of Aeronautics,1(36):178-190
.Effects of Asymmetric Vane Pitch on Reducing Low-Engine-Order Forced Response of a Turbine Stage.[J]:Aerospace,2022,11(9)
.A Modified Shielding and Rapid Transition DDES Model for Separated Flows:Entropy,2022,1(25)
.Forced Response Analysis of an Embedded Compressor Rotor Induced by Stator Disturbances and Rotor–Stator Interactions.[J]:Aerospace,2023,1(10)
.Low-Engine-Order Forced Response Analysis of a Turbine Stage with Damaged Stator Vane.[J]:Entropy,4(26)
.Effect of Intake Acoustic Reflection on Blade Vibration Characteristics.[J]:Aerospace,2024,5(11)
.Fast-moving Mesh Method and Its Application to Circumferential Non-uniform Tip Clearance in a Single-stage Turbine.[J]:Journal of Applied Fluid Mechanics,2024,8(17):1759–1773

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