北京航空航天大学主页平台系统徐旭--中文主页-- [8] X. Wang, Y. Yang, Y. Liu, X. Xu, Q. Yang, Thermodynamic analysis of a high Mach number scramjet engine with secondary combustion for thrust enhancement, Therm. Sci. Eng. Prog. 47 (2024) 102275. https://doi.org/10.1016/j.tsep.2023.102275.

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个人信息

徐旭Xu Xu

教授

教授博士生导师硕士生导师

电子邮箱：

所在单位：宇航学院

学历：博士研究生

办公地点：沙河主楼D座521

在职信息：在职

主要任职：宇航推进系主任

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[8] X. Wang, Y. Yang, Y. Liu, X. Xu, Q. Yang, Thermodynamic analysis of a high Mach number scramjet engine with secondary combustion for thrust enhancement, Therm. Sci. Eng. Prog. 47 (2024) 102275. https://doi.org/10.1016/j.tsep.2023.102275.

发布时间：2024-06-24 点击次数：

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上一条：[7] X. Wang, X. Xu, Q. Yang, Numerical analysis on thermal environment of reusable launch vehicle during supersonic retropropulsion, Int. J. Therm. Sci. 198 (2024) 108857. https://doi.org/10.1016/j.ijthermalsci.2023.108857.

下一条：[9] Xu Wang, Xu Xu, Qingchun Yang, et al. Experimental Study on Fuel Supply Characteristics of Magnesium Powder Ramjet Engine,74th International Astronautical Congress, 2023.