M. Ahmadi and F.A. Khosravi, CFD simulation of non-Newtonian two-phase fluid flow through a channel with
a cavity, Thermal Sci. 24(2B) (2020) 1045–1054.
 M. Ahmadi, S.A.A. Mirjalily and S.A.A. Oloomi, RANS K − ω simulation of 2d turbulent natural convection in
an enclosure with heating sources, IIUM Engin. J. 20(1) (2019) 229–244.
 A.R. AlAli and I. Janajreh, Numerical simulation of turbine blade cooling via jet impingement, Energy Procedia
75 (2015) 3220–3229.
 M. Alhajeri and H. Alhajeri, Heat and fluid flow analysis in gas turbine blade cooling passages with semicircular
turbulators, Int. J. Phys. 4 (2009) 835–845.
 A.A. Amell and F.J. Cadavid, Influence of the relative humidity on the air cooling thermal load in gas turbine
power plant, Appl. Thermal Eng. 22(13) (2002) 1533–1529.
 F. Bazdidi-Tehrani and A. Mahmoodi, Investigation of the effect of turbulence intensity and injection angle on
the flow and temperature field in the single hole film cooling technique, Int. J. Eng. Sci. 4(12) (2002) 25–38.
 S.H. Bhavnani and A.E. Bergles, Interferometric Study of Laminar Natural Convection from An Isothermal
Vertical Plate with Transverse Roughness Elements, PHD Dissertation, Iowa State University, Iowa, 1987.
 M. Choi, H.S. Yoo, G. Yang, J.S. Lee and D.K. Sohn, Measurements of impinging jet flow and heat transfer on
a semi-circular concave surface, Int. J. Heat Mass Transfer 43(10) (2000) 1822–1811. J. Cleeton, R. Kavanagh and G. Parks, Blade cooling optimisation in humid-air and steam-injected gas turbines,
Appl. Thermal Eng. 29(16) (2009) 3283–3274.
 M. Colins, S.J. Harrison, D. Naylor and P.H. Oosthuizen, Heat transfer from an isothermal vertical surface with
adjacent heated horizontal louvers: Numerical analysis, J. Heat Transfer 124 (2002) 1072–1077.
 C. Du, L. Li, X. Wu and Z. Feng, Effect of jet nozzle geometry on flow and heat transfer performance of vortex
cooling for gas turbine blade leading edge, Appl. Thermal Eng. 48(7) (2015).
 A. Ghobadi, M. Javadi and B. Rahimi, Cooling turbine blades using exciting boundary layer, World Academy Sci.
Technol. 62 (2010).
 W. Haas, W. Rodi and B. Schonung, The influence of density difference between hot and coolant gas on film
cooling by a row of holes: Prediction and experiments, ASME J. Turbo Machin. 114 (1992) 755–747.
 J. Horlock, D. Watson and T. Jones, Limitations on gas turbine performance imposed by large turbine cooling
flows, J. Eng. Gas Turb. Power 123(3) (2001) 494–487.
 K.M. Kim, J.S. Park, D.H. Lee, T.W. Lee and H.H. Cho, Analysis of conjugated heat transfer, stress and failure
in a gas turbine blade with circular cooling passages, Engin. Failure Anal. 18(4) (2011) 1212–1222.
 C. Langowsky and D.T. Vogel, Influence of film cooling on the secondary flow in a turbine nozzle, AIAA 35(1)
 S.-J. Li, J. Lee, J.-C. Han, L. Zhang and H.-K. Moon, Influence of mainstream turbulence on turbine blade
platform cooling from simulated swirl purge flow, Appl. Thermal Eng. 101 (2016) 678–685.
 Z. Liu and Z. Feng, Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine
blade leading edge, Int. J. Heat Mass Transfer 54(23–24) (2011) 4959–4949.
 Y. Liu, L. Wang and Z.S. Qian, Numerical investigation on the assistant restarting method of variable geometry
for high Mach number inlet, Aerosp. Sci. Technol. 79 (2018) 647–657.
 Z. Liu, L. Ye, C. Wang and Z. Feng, Numerical simulation on impingement and film composite cooling of blade
leading edge model for gas turbine, Appl. Thermal Eng. 73(2) (2014) 1432–1443.
 W. MacCormack, O.R. Tutty and E. Rogers, Stochastic optimization based control of boundary layer transition,
Control Engin. Practice 10 (2002) 260–243.
 K. Mazaheri, M. Zeinalpour and H.R. Bokaei, Turbine blade cooling passages optimization using reduced conjugate
heat transfer methodology, Appl. Thermal Eng. 103 (2016) 1228–1236.
 A.B. Moskalenkoa and A.I. Kozhevnikova, Estimation of gas turbine blades cooling efficiency, Int. Conf. Industrial
Engin. ICIE, (2016).
 R. Roy, A. Tiwari and J. Corbett, Designing a turbine blades cooling system using a generalize regression genetic
algorithm, CIRP Ann. 52(1) (2003) 415–418.
 H. Sun, S. Bu, Y. Luan, T. Sun and X. Pei, Numerical research on the film cooling gas turbine blade with the
conjugate heat transfer method, Materials Res. Innov. 19(6) (2015) 180–175.
 L. Torbidoni and A.F. Massardo, Analytical blade row cooling model for innovative gas turbine cycle evaluations
supported by semi-empirical air cooled blade data, Proc. ASME Turbo Expo Amsterdam, Netherlands, (2002).
 K. Yu, J. Xu, Z. Lv and G. Song, Inverse design methodology on a single expansion ramp nozzle for scramjets,
Aerosp. Sci. Technol. 92 (2019) 9–19.