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

Zhu Chengxiang.Conceptual design methodology and performance evaluation of turbine-based combined cycle inward-turning inlet with twin-design points.Aerospace Science and Technology,2023,152

CHK,Zhu Chengxiang.A constant pressure differential valve and its controlling characteristics for aero engine.FLOW MEASUREMENT AND INSTRUMENTATION,2023,95

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

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.

ZXG,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.

Zhu Chengxiang.Reflection and transition of planar curved shock waves.Journal of Fluid Mechanics,2023,959

Zhu Chengxiang.Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2023,44(2):

Zhu Chengxiang.Digital Twin System for Propulsion Design of UAVs.Proceedings - VRCAI 2022: 18th ACM SIGGRAPH International Conference on Virtual-Reality Continuum and its Applications in Industry,2022,

Zhu Chengxiang.Analytical model for predicting the length scale of shock/boundary layer interaction with curvature (vol 34, 111701, 2022).Physics of Fluids,2022,35(3):