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张强(教授)

所属单位:上海交通大学航天航空学院

担任职务:

擅长领域:

联系方式:021-34207214 邮箱:登录后查看

时间 毕业院校 学历
2001年-2005 美国犹他大学 博士
1993-1996 大连理工大学 硕士
1989-1993 大连理工大学 本科

主要成就

(1)Li W., Zhang Q., Jiang H., and Lee S. W., 2013, “Squealer tip leakage flow Characteristics in transonic condition,” ASME Journal of Turbomachinery.

(2)Zhang Q. and He Li., 2013, “Tip-Shaping for HP Turbine Blade Aero-Thermal Performance management,” ASME Journal of Turbomachinery.

(3)O’Dowd, D., Zhang, Q., He, L., Cheong, B., Tibbet I., 2012, “Aero-Thermal Performance of a Cooled Winglet Tip at Engine Representative Mach and Reynolds numbers,” ASME Journal of Turbomachinery

(4)Zhang, Q. and He, L., 2011, “Over-Tip Choking and Its Implications on Turbine Blade Tip Aerodynamic Performance , “ AIAA-Journal of Propulsion and Power, vol 27, No. 5, Sept.-Oct.2011.

(5)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.

(6)O’Dowd, D., Zhang, Q., He, L., Oldfield, M., Ligrani, P.M., and Cheong B.C.Y., Tibbet, I., 2011, “Aero-Thermal Performance of a Winglet Tip at Engine Representative Mach and Reynolds numbers,” ASME Journal of Turbomachinery, October 2011, Vol 133, 041026-1-8

(7)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

(8)D’Dowd, D.O., Zhang Q., Ligrani, P. M., He, L., and Friedrichs, S., 2011, Comparisons of Heat Transfer Measurement Techniques on a Transonic Turbine Blade Tip, ASME Journal of Turbomachinery, April 2011, Vol 133, 021028-1-10

(9)Thermal Performance of Dimpled Surfaces in Laminar Flows, N. Xiao, Q. Zhang, P. M. Ligrani, R. Mongia, International Journal of Heat and Mass Transfer, March 2009.

(10)Numerical Predictions of Heat Transfer and Flow Characteristics of Heat Sinks With Ribbed and Dimpled Surfaces In Laminar Flow, H. Wee, Q. Zhang, P.M. Ligrani, S. Narasimhan, Numerical Heat Transfer, Part A: Applications, Part A, 53: 1–20, 2008.

(11)Aerodynamic Losses of a cambered Turbine Vane: Influences of Surface Roughness and Freestream Turbulence Intensity, (Q. Zhang and P. M. Ligrani), ASME-Journal of Turbomachinery, Vol. 128, No. 3, pp. 536-546, July 2006.

(12)Influence of Surface Roughness on the Aerodynamic Performance of a Turbine Vane, (Q. Zhang, M. Goodro, P. M. Ligrani, R. Trindade (Pratt & Whitney), S. Sreekanth(Pratt & Whitney-Canada)), ASME -J. Fluids Eng., Vol. 128, No. 3, pp 568-578, May 2006.

(13)Predictions of Stanton Numbers, Skin Friction Coefficients, Aerodynamic Losses, and Reynolds Analogy Behavior for a Transonic Turbine Vane, (Q. Zhang and P. M. Ligrani), Numerical Heat Transfer, Part A: Applications, Volume 49, Number 3, Pages: 237 – 256 February 2006

(14)Wake Turbulence Structure Downstream of a Cambered Airfoil in Transonic Flow: Effects of Surface Roughness and Freestream Turbulence Intensity, (Q. Zhang and P. M. Ligarni), International Journal of Rotating Machinery, Volume 2006, Pages 1–13, 2006.

(15)Comparison of Flow Structure above Dimpled Surfaces with Different Dimple Depths in a Channel, (Se Youl Won, Q. Zhang and P. M. Ligrani), Physics of Fluids, 17, No. 4, pp. 045105-1-9, April 2005.

(16)Mach Number and Freestream Turbulence Effects on the Aerodynamic Losses of a Turbine Vane, (Q. Zhang, D. Sandberg and P. M. Ligrani), AIAA Journal of Propulsion and Power, Vol. 21, No. 6, Nov-Dec., 2005.

(17)Effects of Surface Roughness and Turbulence Intensity on the Aerodynamic Losses Produced by the Suction Surface of a Simulated Turbine Airfoil, (Q. Zhang, S. W. Lee, and P. M. Ligrani), ASME -Journal of Fluids Engineering, Vol. 126, No. 2, pp. 257-265, March 2004.

(18)Mach Number/Surface Roughness Effects on Transonic Turbine Airfoil Aerodynamic Losses, (Q. Zhang, and P. M. Ligrani), AIAA Journal of Propulsion and Power, Vol. 20, No. 6, pp. 1117-1125, November-December, 2004.

(19)Effect of Surface Roughness and Freestream Turbulence on the Wake Turbulence Structure of a Symmetric Airfoil (Q. Zhang, S. W. Lee, and P. M. Ligrani), Physics of Fluids, 16, pp. 2044-2053, 2004.

(20)Determination of Rough-Surface Skin Friction Coefficients from Wake Profile Measurements, (Q. Zhang, S. W. Lee, and P. M. Ligrani), Experiments in Fluids, Vol. 35, No. 6, pp. 627-635, December 2003.

软件版权登记及专利

(1)An Aerofoil Structure: over-tip shaping” , He L, Zhang Q., Wheeler A., Atkins N. UK patent application no. GB1017797.0, Oct. 21, 2010 , European patent application EP11184088.0. Oct. 6, 2011, US patent application no. US 13/269,113. Oct. 7, 2011

(2)“Shaped Squealer Blade Tip for Cooling Equipment”, He L., Zhang Q. UK patent application no GB1223193.2, 21 December 2012