周胜兵，副研究员，硕士生导师。从事爆震发动机技术、涡喷发动机技术、火箭发动机技术等方面的研究和教学工作。2020年国家博新计划获得者。 

2015.09-2020.06   南京理工大学   航空宇航推进理论与工程   博士

2018.09-2019.09   新加坡国立大学   流体力学   博士联合培养

2025.12-至今 重庆大学   航空航天学院   副研究员

2020.06-2025.12 重庆大学   航空航天学院   弘深青年教师教师

1. 国家自然科学基金青年基金，2024.01-2026.12，主持。

2. 国家博士后创新人才支持计划，2020.08-2023.08，主持.

3. 国家博士后资助计划（B类），2024.07-2026.07， 主持.

4. XX科技委基础加强技术领域基金，2021.10-2024.10, 主持。

5. XX装备十四五预研项目，2023.10-2025.10，主持。

6. 重庆市博士后留渝项目，2024.01-2026.12，主持.

1. Zhou S, Wang R, Liu F, Ning H, Hu N. Experimental study on propagation characteristics of rotating detonation wave with ethanol-hydrogen fuel. FUEL. 2026; 407:137579.

2. Wang R, Zhou S*. Study on a combustor of rotating detonation turbine engine with a jet-cooling structure[J]. Case Studies in Thermal Engineering, 2025,72: 106456.

3. Liu G, Wang Z, Zhou S*, et al. Experimental study on effects of nozzles and combustors on the rotating detonation rocket engine in pulse operation[J]. Results in Engineering, 2025,27: 105974.

4. Meng, B, Xia, Z, Zhou S, et al. Numerical investigation of a two-phase non-premixed n-decane/air rotating detonation combustor with inlet-integrated slot film cooling. Applied Thermal Engineering, 281, 128620.

5. Zhou S, Wang R Liu F et al. Effects of liquid-fuel temperature on rotating-detonation-wave propagation[J]. Acta Astronautica, 2024, 223: 134-143.

6. Zhou S, Wang R Liu F et al. Experimental investigation on propagation characteristics of rotating detonation wave fueled by diesel[J]. Acta Astronautica, 2024, 225: 949-959.

7. Zhou S, Liu F, Ning H et al. Experimental investigation on a rotating detonation combustor with the pulse operating frequency of 10 Hz[J]. Acta Astronautica, 2024, 215: 642-652.

8. Dai, C, Sun, B, Zhou S, et al. Numerical investigations on flow and heat transfer characteristics of a high-enthalpy double-cone in thermal and chemical non-equilibrium for hypersonic propulsion. International Communications in Heat and Mass Transfer, 155, 107522.

9. Zhou S, Ma H, Ma Y et al. Experimental investigation on pulse operation characteristics of rotating detonation rocket engine[J]. Fuel, 2023, 354, 129408.

10. Zhou S, Ma Y, Liu F et al. Effects of a straight guide vane on the operating characteristics of rotating detonation combustor[J]. Acta Astronautica, 2023, 203: 135-145.

11. Zhou S, Ma H, Ma Y et al. Investigation on C2H4-Air combustion mode in a non-premixed rotating detonation combustor[J]. Propulsion and Power Research, 2022, 11（1）: 85-96.

12. Ma Y, Zhou S*, Ma H et al. Experimental investigation on propagation characteristics of liquid-fuel/preheated-air rotating detonation wave[J]. International Journal of Hydrogen Energy, 2022, 47（57）: 24080-24092.

13. Dai, C, Sun, B, Zhou, S,. Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet. Acta Astronautica, 193, 237-254.

14. Dai, C, Sun, B, Zhou, S. Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow. Aerospace Science and Technology, 124, 107526.

15. Zhou S, Ma H, Zhou C et al. Experimental research on the propagation process of rotating detonation wave with a gaseous hydrocarbon mixture fuel[J]. Acta Astronautica, 2021, 179: 1-10.

16. Zhou S, Ma H, Ma Y et al. Experimental investigation on detonation wave propagation mode in the start-up process of rotating detonation turbine engine[J]. Aerospace Science and Technology, 2021, 111: 106559.

17. Dai, C, Sun, B, Zhou, S. Numerical investigation of real-gas effect of inward-turning inlet at Mach 12. Aerospace Science and Technology, 115, 106786.

18. Zhou S, Ma H, Yang Y, et al. Investigation on propagation characteristics of rotating detonation wave in a radial-flow turbine engine combustor model [J]. Acta Astronautica, 160, pp. 15-24, 2019.

19. Zhou S, Ma H, Chen S, et al. Experimental investigation on propagation characteristics of rotating detonation wave with a hydrogen-ethylene-acetylene fuel [J]. Acta Astronautica, 157, pp. 310-320, 2019.

20. Zhou, S, Ma, H, Liu, C, et al.Experimental investigation on the temperature and heat-transfer characteristics of rotating-detonation-combustor outer wall [J]. International Journal of Hydrogen Energy, 43(45), pp. 21079-21089, 2018.

21. Zhou S, Ma H, Ma Y, et al.Experimental study on a rotating detonation combustor with an axial-flow turbine[J]. Acta Astronautica, 151, pp. 7-14, 2018.

22. Zhou S, Ma H, Li S, et al.Experimental study of a hydrogen-air rotating detonation engine with variable air-inlet slot [J]. International Journal of Hydrogen Energy, 43(24), pp. 11253-11262, 2018.

23. Zhou S, Ma H, Li S, et al. Effects of a turbine guide vane on hydrogen-air rotating detonation wave propagation characteristics[J]. International Journal of Hydrogen Energy, 42(31), pp. 20297-20305, 2017.

24. Zhou S, Ma H, Liu D, et al. Experimental study of a hydrogen-air rotating detonation combustor[J]. International Journal of Hydrogen Energy, 42(21), pp. 14741-14749, 2017.

25. 周胜兵, 王栋, 马虎, 等. 氧化剂喷注面积对旋转爆震波传播特性影响的实验研究[J]. 推进技术. 38(11), pp. 2634-2640, 2017.

26. 刘事成，高春雨，周胜兵*. 非均匀当量比对旋转爆轰燃烧室性能影响的三维数值模拟研究[J]. 爆炸与冲击. 2024, 44(5): 052101.