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.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,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-.

QRF,YYC,Zhu Chengxiang.Lattice Boltzmann simulation for high-speed compressible viscous flows with a boundary layer.Applied Mathematical Modelling,2016,48567-583.

QRF,YYC,Zhu Chengxiang.Three-dimensional coupled double-distribution-function lattice Boltzmann models for compressible Navier-Stokes equations.PRAMANA-JOURNAL OF PHYSICS,2016,89(6):

Zhu Chengxiang,高超声速进气道的裂解碳氢燃料提前喷注.第九届全国流体力学学术会议论文摘要集,2016,1.

Zhu Chengxiang,Direct numerical simulation of a non-Newtonian liquid jet in crossflow.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2016,37(9):2659-2668.

YYC,剪切稀化流体的撞击破碎数值分析.2016海峡两岸流体力学研讨会论文摘要集,2016,1.

Zhu Chengxiang,非牛顿撞击射流破碎的直接数值模拟.中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议论文集,2016,8.