Zhu Chengxiang,YYC,Direct numerical simulation of impinging jet with non-Newtonian shear thinning properties at high ambient pressure.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2019,40(6):

一种涡轮基组合动力的整机低速风洞试验研究.推进技术,2019,

Zhu Chengxiang,高压环境下剪切稀化非牛顿撞击射流直接数值模拟.航空学报,2019,40(6):143-152.

Zhu Chengxiang,高压环境下剪切稀化非牛顿撞击射流直接数值模拟.航空学报,2019,10.

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.