Zhu Chengxiang,Numerical investigation of fuel pre-injection with different injector configurations in hypersonic inlet.21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,

Zhu Chengxiang,SCG,Analytical reconstruction of axisymmetric curved shock wave/boundary layer interactions.Physics of Fluids,2024,36(4):

Zhu Chengxiang.Reflection and transition of planar curved shock waves.Journal of Fluid Mechanics,2023,959

Zhu Chengxiang.Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2023,44(2):

Zhu Chengxiang.Digital Twin System for Propulsion Design of UAVs.Proceedings - VRCAI 2022: 18th ACM SIGGRAPH International Conference on Virtual-Reality Continuum and its Applications in Industry,2022,

SCG,Zhu Chengxiang.Analytical model for curved-shock Mach reflection.Physics of Fluids,2022,35(3):

Zhu Chengxiang.Analytical model for predicting the length scale of shock/boundary layer interaction with curvature (vol 34, 111701, 2022).Physics of Fluids,2022,35(3):

KXJ,Zhu Chengxiang,Analytical model for predicting the length scale of shock/boundary layer interaction with curvature.Physics of Fluids,2022,34(11):

YYC,基于三维弯曲激波的宽域变马赫数乘波体设计分析.南京航空航天大学学报,2022,54(05):937-948.

Zhu Chengxiang.Theoretical model of 2D curved shock wave/turbulent boundary layer interaction.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2022,43(9):