个人简介

周超，研究员、博士生导师、北京大学航空航天工程系副系主任、叶轮机械实验室主任、北京大学工程科学与新兴技术高精尖创新中心仿真与应用软件部Co-PI。周超于2003年本科毕业于南京航空航天大学，2010年博士毕业于剑桥大学，专业方向为叶轮机械气动和传热。之后回国到北京大学任教至今，一直从事该方向研究。周超研究的主要对象为涡轮。在领域内顶级期刊Journal of Turbomachinery上发表了9篇论文。周超针对针对高压涡轮中的叶顶泄漏流、过渡段、低压涡轮和气膜冷却等关键技术开展了研究工作。负责了国家自然科学基金重大研究计划培育项目、面上项目、青年基金、工信部民机科研子课题、航空科学基金等多个项目。研究水平得到了国内外同行的认可，被担任领域内重要国际会议2019年国际推进与动力北京论坛的大会审稿副主席(review co-Chair)。

代表性著作

1. Zhong, L, Zhou, C.*, Chen, S. Y., “Large Eddy Simulation of Inclined Jet in Cross Flow with Cylindrical and Fan-Shaped Holes,” Journal of Propulsion and Power, 2018, Vol. 34. No. 5., pp. 1098-1108

2. Zhou, K and Zhou, C.*, “Aerodynamic Interaction Between an Incoming Vortex and Tip Leakage Flow in a Turbine Cascade,” Journal of Turbomachinery, 2018, Vol. 140, No. 5, 111004

3. Zhou, C.* and Zhong, F., “A Novel Suction Side Winglet Design Philosophy for High Pressure Turbine Rotor Tips,” Journal of Turbomachinery, 2017, Vol. 139 No.11, pp:111002-111002-11.

4. Zhong, F. and Zhou, C.*, “Effects of Tip Gap Size on the Aerodynamic Performance of a Cavity-winglet Tip in a Turbine Cascade,” Journal of Turbomachinery, 2017, Vol. 139 No.10, pp.101009-101009-9.

5. Zhong, F, and Zhou, C.*, “Tip Gap Size Effects on Thermal Performance of Cavity-winglet Tips in Transonic Turbine Cascade with Endwall Motion,” 2017, Journal of the Global Power and Propulsion Society, 2017, Vol. 1, pp41-45

6. 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.

7. 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.

8. 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.

9. Zhou, C*, Hodson, H., and Himmel, C., “The Effects of Trailing Edge Thickness on the Losses of Ultrahigh Lift Low Pressure Turbine Blades,” Journal of Turbomachinery, 2014, Vol. 136, No.8, 081011.

10. 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.

11. 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.

12. 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.

13. 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.

14. Zhou, C.*, Hodson, H., and Lock, G., "Thermal Performance of Cooled Tips in a High-Pressure Turbine Cascade," Journal of Propulsion and Power, 2012, Vol. 28, No. 5, pp. 900-911.

15. Zhou, C.*, and Hodson, H., "Squealer Geometry Effects on Aerothermal Performance of Tip-Leakage Flow of Cavity Tips," Journal of Propulsion and Power, 2012, Vol.28, No.3, pp.556-567.