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周超
Researcher 航空航天工程系副系主任 Supervisor of Doctorate Candidates Supervisor of Master's Candidates
Email:
264a1fe91ff4b11278161abadf6651abf2677eba4bab325f326326040fdb18f96ee8d58d508540f0e253820654ca3753bd7d33b42952098c2a4cb2834136e0e504304306332a4ad9731bcc854ace29f873c14e91a2fb050975d540448a0a587057722b7000ebf2244f9be9f58d5f9e7b596621cac71ab2335daa5c87900ea092
Business Address: 北京大学新奥工学大楼
Educational Experience:
1999.1-2003.1
南京航空航天大学 ， 能源与动力学院 ， Bachelor's degree ， 学士
1003.1-1006.1
南京航空航天大学 ， 能源与动力学院 ， 硕士 ， 硕士
2006.1-2010.1
英国剑桥大学 ， 工程系Whittle实验室 ， Doctoral degree ， With Certificate of Graduation for Doctorate Study
Background:
2011.1-2014.1 航空航天工程系 ， 北京大学工学院 ， 特聘研究员、博导
2014.2-Now 航空航天工程系 ， 北京大学工学院 ， 研究员、博导
Award:
Paper:
1.
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.
2.
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.
3.
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.
4.
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.
5.
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.
6.
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
7.
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.
8.
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.
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., 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.
11.
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. 14. Zhou, C*, Hodson, H., and Himmel, C., “The Effects of Trailing Edge Thickn
12.
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.
13.
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.
14.
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.
15.
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.
16.
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.
17.
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
18.
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, 2017, Vol.30 No. 3 pp.939-950.
19.
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.
20.
Zhou, C.* and Zhong, F., “A Novel Suction Side Winglet Design Philosophy for High Pressure Turbine Rotor Tips,” J. Turbomach., 2017, Vol. 139 No.11, pp:111002-111002-11.
21.
Hu, S., Zhou, C.*, Xia, Z., and Chen S. Y., “LES and CDNS Investigation of T106C Low Pressure Turbine”, Journal of Fluid Engineering, 2017, Vol. 140, No.1, 011108.
22.
Hu, S., Zhou, C.*, and Chen, S., “Large Eddy Simulation of Secondary Flows in an Ultra-high Lift Low Pressure Turbine Cascade at Various Inlet Incidences,” International Journal of Turbo and Jet Engines, Accepted.
23.
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, Accepted.
