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个人信息Personal Information
助理研究员
硕士生导师
教师英文名称：Shengbing Zhou
教师拼音名称：zhoushengbing
电子邮箱：
入职时间：2020-06-01
所在单位：航空航天学院
学历：研究生(博士后)
性别：男
学位：博士学位
在职信息：在职
毕业院校：南京理工大学
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爆震燃烧及其推进技术；发动机内流动与燃烧.
- ,,,,,,.Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow:AEROSPACE SCIENCE AND TECHNOLOGY,2022,124):-
- ,,,,,,.Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet:ACTA ASTRONAUTICA,2022,193):237-254
- ,,,,.<p>Investigation on C2H4-Air combustion mode in a non-premixed rotating detonation combustor</p>:PROPULSION AND POWER RESEARCH,11):85-96
- ,,,,.Experimental investigation on detonation wave propagation mode in the start-up process of rotating detonation turbine engine:AEROSPACE SCIENCE AND TECHNOLOGY,2021,111):-
- ,,,,,,.Numerical investigation of real-gas effect of inward-turning inlet at Mach 12:AEROSPACE SCIENCE AND TECHNOLOGY,2021,115):-
- ,,,.Experimental research on the propagation process of rotating detonation wave with a gaseous hydrocarbon mixture fuel:ACTA ASTRONAUTICA,2021,179):1-10
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