S.W. Lee, S.U. Kim, K.H. Kim, Aerodynamic performance of winglets covering the tip gap inlet in a turbine cascade, International Journal of Heat and Fluid Flow, 34 (2012) 36-46.
 S. Naik, C. Georgakis, T. Hofer, D. Lengani, Heat transfer and film cooling of blade tips and endwalls, Journal of Turbomachinery, 134(4) (2012) 041004.
 S. Acharya, H. Yang, S.V. Ekkad, C. Prakash, R. Bunker, Numerical simulation of film cooling on the tip of a gas turbine blade, in: ASME Turbo Expo 2002: Power for Land, Sea, and Air, American Society of Mechanical Engineers Digital Collection, 2002, pp. 1051-1062.
 J. Christophel, K.A. Thole, F. Cunha, Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part II: Heat Transfer Measurements, J. Turbomach., 127(2) (2005) 278-286.
 H. Nasir, S.V. Ekkad, R.S. Bunker, Effect of tip and pressure side coolant injection on heat transfer distributions for a plane and recessed tip, Journal of Turbomachinery, 129(1) (2007) 151-163.
 M. Rezasoltani, K. Lu, M.T. Schobeiri, J.-C. Han, A combined experimental and numerical study of the turbine blade tip film cooling effectiveness under rotation condition, Journal of Turbomachinery, 137(5) (2015) 051009.
 Y.C. Nho, Y.J. Lee, J.S. Kwak, Effects of tip shape on the gas turbine blade tip heat transfer, Journal of Thermophysics and Heat Transfer, 26(2) (2012) 305-312.
 J.S. Park, D.H. Lee, D.-H. Rhee, S.H. Kang, H.H. Cho, Heat transfer and film cooling effectiveness on the squealer tip of a turbine blade, Energy, 72 (2014) 331-343.
 F. Cheng, H. Chang, J. Zhang, X. Tian, Effect of film-hole configuration on film-cooling effectiveness of squealer tips, Journal of Thermal Science and Technology, 12(1) (2017) JTST0004-JTST0004.
 E. Eckert, Analysis of film cooling and full-coverage film cooling of gas turbine blades, Journal of Engineering for Gas Turbines and Power, 106(1) (1984) 206-213.
 D.G. Bogard, K.A. Thole, Gas turbine film cooling, Journal of propulsion and power, 22(2) (2006) 249-270.
 H. Consigny, B. Richards, Short duration measurements of heat-transfer rate to a gas turbine rotor blade, Journal of Engineering for Power, 104(3) (1982) 542-550.
 E. Eckert, Similarity analysis of model experiments for film cooling in gas turbines, Wärme-und Stoffübertragung, 27(4) (1992) 217-223.
 O. Hassan, I. Hassan, Experimental investigations of the film cooling effectiveness of a micro-tangential-jet scheme on a gas turbine vane, International Journal of Heat and Mass Transfer, 61 (2013) 158-171.
 R.J. Moffat, Describing the uncertainties in experimental results, Experimental thermal and fluid science, 1(1) (1988) 3-17.
 F.-n. Cheng, J.-z. Zhang, H.-p. Chang, J.-y. Zhang, Investigations of film-cooling effectiveness on the squealer tip with various film-hole configurations in a linear cascade, International Journal of Heat and Mass Transfer, 117 (2018) 344-357.
 K. He, Investigations of film cooling and heat transfer on a turbine blade squealer tip, Applied Thermal Engineering, 110 (2017) 630-647.
 I. Sadrehaghighi, Essentials of Turbomachinery in CFD, 2019.
 H. Li, X. Su, X. Yuan, Entropy Analysis of the Flat Tip Leakage Flow with Delayed Detached Eddy Simulation, Entropy, 21(1) (2019) 21.
 L. Kavurmacioglu, H. Maral, C.B. Senel, C. Camci, Performance of partial and cavity type squealer tip of a HP turbine blade in a linear cascade, International Journal of Aerospace Engineering, 2018 (2018).
 W. Li, W.-y. Qiao, K.-f. Xu, H.-l. Luo, Numerical simulation of tip clearance flow passive control in axial turbine, Journal of Thermal Science, 17(2) (2008) 147-155.
 H. Ma, L. Wang, Experimental study of effects of tip geometry on the flow field in a turbine cascade passage, Journal of Thermal Science, 24(1) (2015) 1-9.
 H. Maral, C.B. Senel, L. Kavurmacioglu, C. Camci, Aerothermal performance of partial and cavity squealer tip in a linear turbine cascade, in: Proceedings of the 2nd International Conference on Advances in Mechanical Engineering, Istanbul, Turkey, 2016.
 J.S. Kwak, J.-C. Han, Heat transfer coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade, Journal of Turbomachinery, 125(4) (2003) 648-657.
 Z. Zhou, S. Chen, W. Li, S. Wang, Thermal performance of blade tip and casing coolant injection on a turbine blade with cavity and winglet-cavity tip, International Journal of Heat and Mass Transfer, 130 (2019) 585-602.
 J. Kim, W. Seo, M. Bang, S.H. Kim, S.M. Choi, H.H. Cho, Effect of Shelf Squealer Tip Configurations on Film Cooling Effectiveness, in: ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, American Society of Mechanical Engineers Digital Collection, 2018.