周超

博士、特聘研究員


葉輪機械實驗室主任


聯系電話:010-62751825
電子郵箱:[email protected]
個人主頁:http://www2.coe.pku.edu.cn/subpaget.asp?id=405



工作經歷:

2014.02-至今:北京大學工學院 航空航天工程系 研究員、博導
2011.01-2014.01:北京大學工學院 航空航天工程系 特聘研究員、博導

 

教育經歷:

2006年 - 2010年 英國劍橋大學機械工程系,Whittle實驗室,渦輪機械專業,博士
2003年 - 2006年 南京航空航天大學能源與動力學院工程熱物理 碩士
1999年 - 2003年 南京航空航天大學能源與動力學院 熱能與動力工程 學士

 

研究領域:

1. 航空發動機
2. 葉輪機械中的空氣動力學和傳熱學問題

 

期刊論文(*為通訊作者):

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.  周凱,周超*,鐘芳盼,“跨聲速葉柵中氣膜冷卻對平面葉尖流動和傳熱特性的影響,” 航空動力學報,2013,28(11):2440~2447

13.  鐘芳盼,周超*,周凱, “跨聲速渦輪中兩種葉片葉尖泄漏流的氣動性能,” 航空動力學報,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,毛軍逵, “渦輪葉片尾緣斜劈縫氣膜冷卻數值模擬,” 南京航空航天大學學報, 2006年 第38卷, 第5期.

20.  周超, 常海萍, 崔德平, 毛軍逵, “斜劈縫渦輪導向葉片尾緣出流氣體流動特性數值分析,” 航空動力學報, 2006年 第21卷 第02期.

 

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