Zhu Chengxiang,CJP,Machine Learning-Based Backpressure Unstart Prediction and Warning Method for Combined Cycle Engine Hypersonic Inlet-Oriented Wide Speed Range.INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,2024,2024

Zhu Chengxiang.Conceptual Design Methodology and Performance Evaluation of Inward-Turning Tbcc Inlet with Twin-Design Points.SSRN,2024,

Zhu Chengxiang,SCG,Mach reflection of three-dimensional curved shock waves on V-shaped blunt leading edges.JOURNAL OF FLUID MECHANICS,2023,975

Zhu Chengxiang.Thermal insulation characteristics of high-temperature heat seals for hypersonic aero-engines.Journal of Physics: Conference Series,2566(1):

基于局部偏转吻切方法的背部进气高超飞行器一体化设计研究.空天技术,2023,(05):1-10.

引射火箭启动过程的进气道动态特性仿真研究.气动研究与试验,2024,2(02):52-58.

考虑来流边界层的超燃燃烧室喷射特性.航空动力学报,2016,31(06):1351-1358.

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,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,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.