بررسی عملکرد مدل‌های مختلف اغتشاشی در تعیین توزیع فشار بر روی سطح یک پره با زاویه چرخش زیاد

[1] Walsh, P. Fletcher, “Gas turbine performance”, 2nd ed. Fairfield, NJ: Blackwell Science Ltd.and ASME Press; 2004 [chapter 1, pp. 1-60,chapter 8, pp. 345-366].

[2] M. Mahmoodi, M.R. Ansari, “Numerical investigation of turbine blade trailing edge flow ejection effects on mach number distribution of gas turbine blade surface: using RNG k-ε turbulence model”, Mechanical and erospace

Engineering Journal, Vol. 1, No. 2, pp. 47-60,2005

[3] K. Takeishi, M. Matsuura, S. Aoki, T. Sato, “An experimental study of heat transfer and film cooling on low aspect ratio turbine nozzles”, Journal of Turbomachinery 112, pp.448-496, 1990

[4] S. Burguburu, C. Toussaint, G. Leroy, “Numerical optimization for turbomachinery blades aerodynamic design using a gradient method coupled with a Navier-Stokes solver”,ISABE, Vol. 1117, 2001

[5] G. Brereton, T. Shih, “Turbulence modeling in simulation of gas-turbine flow and heat transfer”, ANNALAS of the New York Academy of Sciences journal of Heat Transfer in Gas Turbine Systems, Vol. 934, pp. 52-63,May 2001

[6] S. Goel, J.I. Cofer, H. Singh, “Turbine airfoil design optimization”, ASME paper 96-GT-158,1996

[7] S. Y. Cho, E.S. Yoon, B. S. Choi, “A study on an axial-type 2-D turbine blade shape for reducing the blade profile loss”, KSME International Journal, Vol. 16, No.8, pp. 1154-1164, 2002

[8] Stephen B. Pope; Turbulent Flows, 1 st Edition,Cambridge University Press, 2000

[9] Baldwin, B. S., Lomax, H., “Thin layer approximation and algebraic model for separated turbulent flows”, AIAA 16^th Aerospace Sciences Meeting, Huntsville, Al,January 1978

[10] S. Djouimaa, L. Messaoudi, Paul W. Giel, “Transonic turbine blade loading calculations using different turbulence models: Effects of reflecting and non-reflecting boundary conditions”, Elsevier journal of Applied

Thermal Engineering, No. 27, pp. 779-787,2007

[11] B. Launder, D. Spalding, “The numerical computation of turbulent flows”, Comput.Meth. Appl. Mech. Eng., pp. 269-289, 1974

[12] F. Menter, “Performance of popular turbulence models for attached and separated adverse pressure gradient flows”, AIAA Journal 30(8),pp. 2066-2072, 1992

[13] P. Bradshaw, “Understanding and prediction of turbulent flow”, International journal of heat and fluid flow 18, pp. 45-54, 1997

[14] Shih, W. Liou, A. Shabbir, Z. Yang, J. Zhu, “A new k-ε eddy viscosity model for high Reynolds number turbulent flows: model development and validation, Technical report NASA-TM-106721”, Institute for

Computational Mechanics in Propulsion and Center for Modeling of Turbulence and Transition Lewis Research Center, 1994

[15] F. Menter, “Two-equation eddy-viscosity turbulence models for engineering applications”, AIAA Journal 32(8), pp. 1598-1605, 1994

[16] D. Wilcox; Turbulence Modeling for CFD, 2 nd Edition, DCW Industries, 2000

[17] B. Lakshminarayana, “Fluid Dynamicand Heat Transfer of Turbomachinery”, John Wiley and Sons, New York, 1996

[18] D. Lastiwka, “Influence of rotor blade scaling on the numerical simulation od a high pressure gas turbine” M.A. Thesis, Ottawa-Carleton Institute for Mechanical and Aerospace Engineering University of Ottawa, Ottawa,Ontario, Canada, May 14, 2009

[19] D. Dunn, Snedden, Von Backstrom, “Turbulence model comparisons for a low pressure 1.5 stage test turbine”, 19th Conference of the International Society for Air Breathing Engines, Montreal, Quebec, Canada, 7-11 September 2009

[20] S. W. Lee, B. J. Chae, “Effects of squealer rim height on aerodynamic losses downstream of a high-turning turbine rotor blade”, Elsevier journal of Experimental Thermal and Fluid Science ,doi:10.1016/j.expthermflusci.2008.03.004

[21] I. Celik, J. Li, “Assessment of numerical uncertainty for the calculation of turbulent flow over a backward facing step”, International Numerical Method in Fluids, No.49, pp. 1015-1031, 2005

[22] Ansys (2006), Fluent 6.3 User’s Guide, Ansys Inc.