Education Background
2006 – 2010: Ph.D., Whittle Laboratory, Department of Engineering, University of Cambridge, UK
2003 – 2006: M.Eng., College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, China
1999 – 2003: B.Eng., College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, China
Professional Experience
2010 – Present: Assistant Professor, College of Engineering, Peking University, Beijing, China
Research Areas
1. Turbomachinery: Aerodynamics and Heat Transfer
2. Internal Flow
Awards and Honors
2006-2010 Cambridge Overseas Trust
Professional Activities
- Reviewer, Journal of Turbomachinery
- Reviewer, Journal of Propulsion and Power
- Member, ASME
Selected Publications
1. Zhou, C.*, and 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, Accepted
2. Zhou, C.*, and Hodson, H., Tibbott, I. and Stokes, M., 2012,“Effects of Endwall Motion on the Aero-Thermal Performance of a Winglet Tip in a HP Turbine”, Journal of Turbomachinery, 134, 061036 (12pages)
3. Zhou, C.*, Hodson, H., and Lock, G., 2012, "Thermal Performance of Cooled Tips in a High-Pressure Turbine Cascade," Journal of Propulsion and Power, Vol. 28, No. 5, pp. 900-911
4. Zhou, C.*, and Hodson, H., 2012 "Squealer Geometry Effects on Aerothermal Performance of Tip-Leakage Flow of Cavity Tips," Journal of Propulsion and Power, Vol.28, No.3, pp.556-567
5. Zhou, C.*, and Hodson, H., 2011, “The Tip Leakage Flow of an Unshrouded High Pressure Turbine Blade with Tip Cooling”, Journal of Turbomachinery, Vol.133, Issue 4, 041028(12 pages)
6. Zhou, C.*, and Hodson, H., 2009, “Numerical Investigation of Thermal Performance of Unshrouded HP Turbine Blade Tips,” International Journal of Turbo and Jet Engines, Vol.26, pp. 277-284
*Corresponding Author