[1] حسینعلی پور س م، شهبازیان ح، قبادی م، نوروزی م ص (1397) آنالیز سیالاتی-حرارتی اثرات دوران و بویانسی دورانی در خنککاری داخلی پرههای توربین گاز. مطالعه آزمایشگاهی مجله علمی و پژوهشی مکانیکسازههاو شارهها 288-277 :(3)8.
[2] Tan X, Zhou X, Shan Y, Zhang J (2019) Analysisof heat transfer on film cooling performance in a flat plate. Energy Proced 158: 4154-4159.
[3] Silieti M, Kassab AJ, Divo E (2009) Film cooling effectiveness: comparison of adiabatic and conjugate heat transfer CFD models. Int J Therm Sci 48(12): 2237-2248.
[4] Karcz MI (2006) Mean and turbulent thermal fields due to film cooling via an eddy heat diffusivity closure. Task Quarterly 10(4): 377-390.
[5] Ochrymiuk T (2016) Numerical prediction of film cooling effectiveness over flat plate using variable turbulent prandtl number closures. J Therm Sci 25(3): 280-286.
[6] تجلی س م، محمدی ا، منتظری م (1392) مدلسازی و شبیهسازی توربین گازی دو محوره با در نظرگیری اثرات خنککاری پرههای توربین. مجله علمی و پژوهشیمکانیکسازههاوشارهها 101-89 :(4)3.
[7] Park JS, Lee DH, Rhee DH, Kang SH, Cho HH (2014) Heat transfer and film cooling effectiveness on the squealer tip of a turbine blade. Energy 72: 331-343.
[8] Lutum E, Von Wolfersdorf J, Semmler K, Dittmar J, Weigand B (2001) An experimental investigation of film cooling on a convex surface subjected to favourable pressure gradient flow. Int J Heat Mass Tran 44(5): 939-951.
[9] Guo X, Schröder W, Meinke M (2016) Large-eddy simulations of film cooling flows. Comput Fluids 35(6):587-606.
[10] Qin Y, Chen P, Ren J, Jiang H (2016) Effects of wall curvature and streamwise pressure gradient on film cooling effectiveness. App Therm Eng 107: 776-784.
[11] Colban W, Gratton A, Thole KA, Haendler M (2006) Heat transfer and film-cooling measurements on a stator vane with fan-shaped cooling holes. J Turbomach 128(1): 53-61.
[12] Gao Z, Narzary DP, Han JC (2009) Film-cooling on a gas turbine blade pressure side or suction side with compound angle shaped holes. J Turbomach 131(1): 11-19.
[13] Liu K, Yang SF, Han JC (2012) Influence of coolant density on turbine blade film-cooling with axial shaped holes. Asme Turbo Expo 757-767.
[14] Li G, Deng H (2011) Experimental investigation on film cooling performance of pressure side in annular cascades. J Therm Sci 20(2): 119.
[15] Zhaoqing K, Wang J (2015) Numerical investigations of pulsed film cooling on an entire turbine vane. App Therm Eng 87: 117-126.
[16] Stenger D, Ghia U, Ou S, Thornburg H (2010) numerical simulation of continuous and pulsed film cooling on a turbine-blade leading-edge model, including surface conductance. In48th AIAA Aero Sciences 1474.
[17] Aga V, Mansour M, Abhari RS (2009) aerothermal performance of streamwise and compound angled pulsating film cooling jets. J Turbomach 131(4): 041015.
[18] حسینی بغدادآبادی س م، زیرک س، رجبی زرگرآبادی م (1397) شبهسازی عددی اثربخشی خنککاری لایهای نوسانی موج سینوسی با توجه به تغییر پارامترهای تزریق خنککننده. مهندسی مکانیک مدرس 200-191 :(1)19.
[19] Ekkad SV, Ou S, Rivir RB (2004) A transient infrared thermography method for simultaneous film cooling effectiveness and heat transfer coefficient measurements from a single test. J Turbomach 126(4): 597-603.
[20] Mack M, Niehuis R, Fiala A, Guendogdu Y (2013) Boundary layer control on a low pressure turbine blade by means of pulsed blowing. J Turbomach 135(5): 051023.
[21] Muldoon F, Acharya S (2010) Direct numerical simulation of pulsed jets-in-crossflow. Comput Fluids 39(10): 1745-1773.
[22] Menter FR, Kuntz M, Langtry R )2003( Ten years of industrial experience with the SST turbulence model. Turbulence Heat Mass Trans 4(1): 625-632.
[23] Hylton LD, Mihelc MS, Turner ER, Nealy DA, York RE (1983) Analytical and experimental evaluation of the heat transfer distribution over the surfaces of turbine vanes. NACA, Report No. CR-168015.