张强 - 上海交通大学

个人简介

教育背景 Ph.D. Mechanical Engineering, University of Utah (2005) M.S. Department of Chemical Machinery, Dalian University of Technology (1996) B.S. Department of Chemical Machinery, Dalian University of Technology (1993) 工作经历 2019 – present Associate Professor (Tenured), UM-SJTU Joint institute, Shanghai Jiao Tong University 2014 – 2019 City, University of London, Mechanical Engineering and Aeronautics, Lecturer 2012 – 2015 Associate Professor, UM-SJTU Joint institute, Shanghai Jiao Tong University 2009 – 2011 Assistant Professor, UM-SJTU Joint institute, Shanghai Jiao Tong University 2006 – 2010 Research Assistant, University of Oxford, UK, Osney Thermo-Fluids Laboratory, Rolls-Royce University Technology Center. 2005 – 2006 Research Assistant Professor, University of Utah 2000 – 2001 Manager, WIKA Beijing Office (Germany instrumentation company)

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Miao X., Zhang Q*.,Atkin C., and Sun Z., 2018, “Improved Purge Air Cooling Effectiveness by Engineered End-Wall Surface Structure – Part 1: Duct Flow,” ASME J Turbomach, Vol. 140 / 091001-1 Miao X., Zhang Q.*,Atkin C., and Sun Z., 2018, “Improved Purge Air Cooling Effectiveness by Engineered End-Wall Surface Structure – Part II: Cascade Flow,” ASME Journal of Turbomachinery, Vol. 140 / 091002-1 Jiang H., Zhang Q*, Lu S., Wang L, and Teng J, 2018, “Experimental Evidence of Temperature Ratio Effect on Turbine Blade Tip Heat Transfer,” ASME Journal of Turbomachinery, 140(12), 121010 (Nov 28, 2018) Zhang Q.* and He L., 2017, “Turbine blade tip aero-thermal management: some recent advances and research outlook,” Journal of the Global Power and Propulsion Society, accepted & in press. (GPPS Best Paper Award) Ma H., Zhang Q.*, Wang L., He L., Wang Z., 2016, “Cooling Injection Effect on a Transonic Squealer Tip – Part 1: Experimental Heat Transfer Results and CFD Validation,” ASME Journal of Engineering for Gas Turbines and Power, 139(5):052506-052506-9, GTP-16-1338 Ma H., Zhang Q.*, Wang L., He L., Wang Z., 2016, “Cooling Injection Effect on a Transonic Squealer Tip – Part 2: Analysis of Aerothermal Interaction Physics,” ASME Journal of Engineering for Gas Turbines and Power, 137(6):062603-062603-7, GTP-14-1541. (ASME Turbo Expo Best Paper Award) Miao X., H Jiang, Zhang Q.*, and Qi H., 2015, “Application of Riblets on Turbine Blade End-wall Secondary Flow Control,” AIAA Journal of Propulsion and Power Vol. 31, No. 6 (2015), pp. 1578-1585. Zhang Q.* and He L., 2013, “Tip-Shaping for HP Turbine Blade Aero-Thermal Performance management,” ASME Journal of Turbomachinery, 135(5) 051025-1-7 Zhang, Q.*, O’Dowd, D., He, L., Wheeler A.P.S., Ligrani, P.M., and Cheong B.C.Y., 2011, “Over-tip shock wave structure and its impact on turbine blade heat transfer,” ASME Journal of Turbomachinery. October 2011, Vol 133, 041001-1-8 Zhang, Q.*, O’Dowd, D., He, L., Oldfield, M., and Ligrani, P.M., 2011, “Transonic Turbine Blade Tip Aero-thermal Performance with Different Tip Gaps: Part I—Tip Heat Transfer,” ASME Journal of Turbomachinery, October 2011, Vol 133, 041027-1-9 Zhang Q. and Ligrani P.M., “Aerodynamic Losses of a cambered Turbine Vane: Influences of Surface Roughness and Freestream Turbulence Intensity,” ASME-Journal of Turbomachinery, Vol. 128, No. 3, pp. 536-546, July 2006.