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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.
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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.
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SCG.A unified transition mechanism from shock to detonation waves.arXiv,2024,
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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):
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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.
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给定光滑三维弯曲激波的乘波体快速逆向设计方法,在研,中国航天基金会,SCG,施崇广,张勐飞,饶洛瑜
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新能源动力推进系统与翼身融合设计方法,在研,SCG,
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三维内转进气道唇口弯曲激波复杂干扰机理研究,在研,SCG,