周胜兵
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
- 代春良,孙波(外),代春良(外),卓长飞(外),周胜兵,周长省(外),YUE LJ(外).Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow:AEROSPACE SCIENCE AND TECHNOLOGY,2022,124):-
- Dai chunliang,Sun bo(外),Dai chunliang(外),周胜兵,Zhuo Changfei(外),Zhou changsheng(外),Yue LJ(外).Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet:ACTA ASTRONAUTICA,2022,193):237-254
- 周胜兵,马虎(外),马元(外),周长省(外),胡宁.<p>Investigation on C2H4-Air combustion mode in a non-premixed rotating detonation combustor</p>:PROPULSION AND POWER RESEARCH,11):85-96
- 周胜兵,马虎(外),马元(外),周长省(外),胡宁.Experimental investigation on detonation wave propagation mode in the start-up process of rotating detonation turbine engine:AEROSPACE SCIENCE AND TECHNOLOGY,2021,111):-
- 代春良,孙波(外),代春良(外),周长省(外),卓长飞(外),杜雷(外),周胜兵.Numerical investigation of real-gas effect of inward-turning inlet at Mach 12:AEROSPACE SCIENCE AND TECHNOLOGY,2021,115):-
- 周胜兵,马虎(外),周长省(外),胡宁.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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