CRQ,Zhu Chengxiang.Numerical Simulation of Aerodynamic Characteristics of Helicopter Rotor with Tip Slots.Transactions of Nanjing University of Aeronautics and Astronautics,2018,35(6):942-951.

YYC,Zhu Chengxiang.Aerodynamic Combination Design Concept for Hypersonic Waverider Forebody and Inward Turning Inlet.Tuijin Jishu/Journal of Propulsion Technology,2018,39(10):2320-2328.

YYC,Zhu Chengxiang.Reversal design of external compression bump of Bump inlet based on osculating cones principle.Hangkong Dongli Xuebao/Journal of Aerospace Power,2018,33(9):2257-2267.

Zhu Chengxiang,YYC,Direct numerical simulation of sheet breakup formed by two impinging jets with non-Newtonian shear thinning properties.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2018,39(5):

QRF,YYC,Zhu Chengxiang.A Hermite-based lattice Boltzmann model with artificial viscosity for compressible viscous flows.INTERNATIONAL JOURNAL OF MODERN PHYSICS B,2018,32(13):

QRF,YYC,Zhu Chengxiang.A double-distribution-function lattice Boltzmann model for high-speed compressible viscous flows.Computers and Fluids,2018,16624-31.

Zhu Chengxiang.Integration design and analysis for curved conical forebody and three-dimensional inward turning inlet.Hangkong Dongli Xuebao/Journal of Aerospace Power,2018,33(1):87-96.

Zhu Chengxiang,YYC,Pre-Injection of Cracked Hydrocarbon Fuel in Hypersonic Inlets.Tuijin Jishu/Journal of Propulsion Technology,2018,39(1):196-202.

Zhu Chengxiang,YYC,Direct numerical simulation of impinging jet breakup with non-Newtonian properties at low Weber number.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2017,38(8):

Zhu Chengxiang,低韦伯数非牛顿射流撞击破碎直接数值模拟.航空学报,2017,38(8):120764-.