工作经历：
2014.02-至今：33678新甫京国际品牌 航空航天工程系 研究员、博导
2011.01-2014.01：33678新甫京国际品牌 航空航天工程系 特聘研究员、博导
教育经历：
2006年 - 2010年 英国剑桥大学机械工程系，Whittle实验室,涡轮机械专业，博士
2003年 - 2006年 南京航空航天大学能源与动力学院工程热物理 硕士
1999年 - 2003年 南京航空航天大学能源与动力学院 热能与动力工程 学士
研究领域：
2006年 - 2010年 英国剑桥大学机械工程系，Whittle实验室,涡轮机械专业，博士
2003年 - 2006年 南京航空航天大学能源与动力学院工程热物理 硕士
1999年 - 2003年 南京航空航天大学能源与动力学院 热能与动力工程 学士
研究领域：
1. 航空发动机
2. 叶轮机械中的空气动力学和传热学问题
期刊论文（*为通讯作者）：
1. Cao, Z., Zhou, C*, and Sun, Z., “The comparison of the aerodynamic characteristics between a novel highly loaded injected blade with curvature induced pressure-recovery concept and a conventional design,” Chinese Journal of Aeronautics, Accepted.
2. Zhong, F., Zhou, C*, Ma, H., and Zhang, Q., “Heat Transfer of Winglet Tips in a Transonic Turbine Cascade,” Journal of Engineering for Gas Turbines and Power, 2017, Vol. 139, pp. 0126051-01260511.
3. Zhong, L., Zhou, C* and Chen S., “Effects of Approaching Main flow Boundary Layer on Flow and Cooling Performance of an Inclined Jet in Cross Flow,” International Journal of Heat and Mass Transfer, 2016, Vol.103, pp: 572-581.
4. Zhou, K., and Zhou, C.*, “Transport Mechanism of Hot Streaks and Wakes in a Turbine Cascade,” Journal of Propulsion and Power, 2016, Vol.32, No.5, pp:1045-1054.
5. Zhou, C.*, “Effects of Endwall Motion on Thermal Performance of Cavity Tips with Different Squealer Width and Height,” International Journal of Heat and Mass Transfer, 2015, Vol. 91, Pages 1248–1258.
6. Zhou,C.*, “Thermal Performance of Transonic Cooled Tips in a Turbine Cascade,” Journal of Propulsion and Power, 2015, Vol. 31, No. 5, pp. 1268-1280.
7. Zhou,C.*, "Aerothermal Performance of Different Tips in Transonic Turbine Cascade with End-Wall Motion", Journal of Propulsion and Power, 2014, Vol. 30, No. 5, pp. 1316-1327.
8. Zhou, C*, Hodson, H., and Himmel, C., “The Effects of Trailing Edge Thickness on the Losses of Ultra-High Lift LP Turbine Blades,” Journal of Turbomachinery, 2014, Vol. 136, No.8, 081011.
9. Luo, J.Q, Zhou, C., and Liu, F.*, “Multipoint Design Optimization of a Transonic Compressor Blade by Using an Adjoint Method,” Journal of Turbomachinery, 2014, Vol. 136, No.5, pp. 051005- 051015.
10. Zhou, C.*, Hodson, H., Tibbott, I. and Stokes, M., “Effects of Winglet Geometry on the Aerodynamic Performance of Tip Leakage Flow in a Turbine Cascade," Journal of Turbomachinery, 2013, Vol. 135, No.5, 051009- 051019.
11. Zhou, C.*, Hodson, H., Tibbott, I. and Stokes, M., “The Aero-thermal Performance of a Cooled Winglet Tip in a High Pressure Turbine Cascade,” Journal of Turbomachinery, 2013, Vol. 135, No.3, 031005- 031015.
12. 周凯，周超*，钟芳盼，“跨声速叶栅中气膜冷却对平面叶尖流动和传热特性的影响,” 航空动力学报，2013，28(11)：2440~2447
13. 钟芳盼，周超*，周凯, “跨声速涡轮中两种叶片叶尖泄漏流的气动性能,” 航空动力学报,2013,28(10):2316~2325.
14. Zhou, C.*, Hodson, H., Tibbott, I. and Stokes, M., “Effects of Endwall Motion on the Aero-Thermal Performance of a Winglet Tip in a HP Turbine,” Journal of Turbomachinery, 2012, Vol. 134, No.6, pp. 061036-061047.
15. Zhou, C.*, Hodson, H., and Lock, G., "Thermal Performance of Cooled Tips in a High-Pressure Turbine Cascade," AIAA Journal of Propulsion and Power, 2012, Vol. 28, No. 5, pp. 900-911.
16. Zhou, C.*, and Hodson, H., "Squealer Geometry Effects on Aerothermal Performance of Tip-Leakage Flow of Cavity Tips," AIAA Journal of Propulsion and Power, 2012, Vol.28, No.3, pp.556-567.
17. Zhou, C.*, and Hodson, H., “The Tip Leakage Flow of an Unshrouded High Pressure Turbine Blade with Tip Cooling”, Journal of Turbomachinery, 2011, Vol.133, No. 4, pp. 041028-041039.
18. Zhou, C.*; Hodson, H.，Numerical Investigation of Thermal Performance of Unshrouded HP Turbine Blade Tips ，International Journal of Turbo and Jet Engines, 2009, Vol. 26, No.4, pp 277-284.
19. 周超, 常海萍,崔德平,毛军逵, “涡轮叶片尾缘斜劈缝气膜冷却数值模拟，” 南京航空航天大学学报, 2006年 第38卷, 第5期.
20. 周超, 常海萍, 崔德平, 毛军逵, “斜劈缝涡轮导向叶片尾缘出流气体流动特性数值分析,” 航空动力学报, 2006年 第21卷 第02期.
