二维弯曲激波/湍流边界层干扰流动理论建模.航空学报,2021,14.

YYC,Zhu Chengxiang.Method of curved-shock characteristics with application to inverse design of supersonic flowfields.JOURNAL OF FLUID MECHANICS,2021,920-.

Zhu Chengxiang.Integration Layout of Double-Modules Chin Inward-Turning Inlet and Conical Forebody.Tuijin Jishu/Journal of Propulsion Technology,2020,42(11):2455-2464.

双模块下颌式内转进气道/圆锥前体一体化布局研究.推进技术,2020,

三维内转TBCC进气道模态转换过程流动分析.第五届空天动力联合会议暨中国航天第三专业信息网第41届技术交流会论文集（第一册）,2020,

Zhu Chengxiang,Direct Numerical Simulation of Breakup Characteristics of Power Law Fluid Impingement Jet.Tuijin Jishu/Journal of Propulsion Technology,2020,41(8):1895-1902.

转级模式对三维内转组合进气道模态转换性能的影响分析.推进技术,2020,41(12):2670-2680.

转级模式对三维内转组合进气道模态转换性能的影响分析.推进技术,2020,

幂律型流体撞击射流破碎特性直接数值模拟.推进技术,2019,8.

YYC,Zhu Chengxiang.Local-Turning Osculating Cones Method for Waverider Design.AIAA JOURNAL,2019,58(8):3499-3513.