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[1]侧滑角对V型钝化唇口激波干扰结构影响研究.航空学报,2024,1-15.
[2]三维弯曲流面法及其在外流乘波体中的应用.航空学报,2024,1-11.
[3]SCG.A unified transition mechanism from shock to detonation waves.arXiv,2024,
[4]张涛,Zhu Chengxiang,SCG,YYC.Fully appreciating the impossibility of shock wave regular reflection from the axis of symmetry in axisymmetric internal flows.Physics of Fluids,2024,36(7):
[5]侧滑角对V型钝化唇口激波干扰结构影响研究.航空学报,2024,1-15.
[6]三维弯曲流面法及其在外流乘波体中的应用.航空学报,2024,1-11.
[7]YYC,SCG.Curved detonation and its reflections.JOURNAL OF FLUID MECHANICS,2024,984
[8]SCG,Zhu Chengxiang,Analytical reconstruction of axisymmetric curved shock wave/boundary layer interactions.Physics of Fluids,2024,36(4):
[9]YYC,SCG.A theoretical method for oblique and curved detonation waves.PHYSICS OF FLUIDS,2023,36(6):
[10]SCG,Zhu Chengxiang,Mach reflection of three-dimensional curved shock waves on V-shaped blunt leading edges.JOURNAL OF FLUID MECHANICS,2023,975
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