## Nomenclature
(2022) [PERSON]; [PERSON]; [PERSON]; [PERSON] Numerical investigation of blowing ratio, density ratio and axial position of film holes on the vane endwall film cooling effectiveness with upstream step. _Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng._**2022**, _236_, 541-553. [CrossRef]
* [PERSON] et al. (2023) [PERSON]; [PERSON]; [PERSON] The Effects of Mainstream Reynolds Number and Blowing Ratio on Film Cooling of Gas Turbine Vanes. _Fluids_**2023**, \(8\), 263. [CrossRef]
* [PERSON] et al. (2025) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] Investigation of the endwall film holes layout strategy based on the conjugate temperature gradient distribution in gas turbine blade cooling. _Appl. Therm. Eng._**2025**, _263_, 125447. [CrossRef]
* [PERSON] (2012) [PERSON]; [PERSON] A Gas Turbine Film Cooling. _J. Propuls. Power_**2012**, _22_, 249-270. [CrossRef]
* [PERSON] et al. (2021) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] Large eddy simulation of pulsed film cooling with vortex generators. _Int. J. Heat Mass Transf._**2021**, _180_, 121806. [CrossRef]
* [PERSON] and [PERSON] (2015) [PERSON]; [PERSON] Numerical investigations of pulsed film cooling on an entire turbine vane. _Appl. Therm. Eng._**2015**, _87_, 117-126. [CrossRef]
* [PERSON] et al. (2025) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] Experimental and computational investigation of the regional endwall cooling performance considering influences of film holes layouts and purge slot shape. _Therm. Sci. Eng. Prog._**2025**, _59_, 103333. [CrossRef]
* [PERSON] et al. (2020) [PERSON]; [PERSON]; [PERSON]; [PERSON] Sweeping Jet Film Cooling at High Blowing Ratio on a Turbine Vane. _J. Turbomach._**2020**, _142_, 121010. [CrossRef]
* [PERSON] et al. (2021) [PERSON]; [PERSON]; [PERSON] A comprehensive review of pulsating flow on heat transfer enhancement. _Appl. Therm. Eng._**2021**, _196_, 117275. [CrossRef]
* [PERSON] et al. (2021) [PERSON]; [PERSON]; [PERSON]; [PERSON] Film cooling in the trailing edge cutback with different land shapes and blowing ratios. _Int. Commun. Heat Mass Transf._**2021**, _125_, 105311. [CrossRef]
* [PERSON] et al. (2021) [PERSON]; [PERSON]; [PERSON] Effects of an incoming vortex on the film cooling jet. _Int. J. Heat Mass Transf._**2021**, _185_, 122323. [CrossRef]
* [PERSON] et al. (2017) [PERSON]; [PERSON]; [PERSON]; [PERSON] Influence of coolant jet pulsation on the convective film cooling of an adiabatic wall. _J. Heat Transf._**2017**, _139_, 022201. [CrossRef]
* [PERSON] (2009) [PERSON]; [PERSON] Influence of Near Hole Pressure Fluctuation on the Thermal Protection of a Film-Cooled Flat Plate. _J. Heat Transfer._**2009**, _131_, 022202. [CrossRef]
* [PERSON] et al. (2020) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] Unsteady vane-rotor secondary flow interaction of the endwall region in a 1.5-stage variable-geometry turbine. _Energy_**2020**, _309_, 133027. [CrossRef]
* [PERSON] et al. (2023) [PERSON]; [PERSON]; [PERSON] The effects of stator-rotor interaction on unsteady characteristics of turbine tip leakage flow. _Aerosp. Sci. Technol._**2023**, _141_, 108544. [CrossRef]
* [PERSON] et al. (2019) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] Combined effects of unsteady wake and free-stream turbulence on turbine blade film cooling with laid-back fan-shaped holes using PSP technique. _Int. J. Heat Mass Transf._**2019**, _133_, 382-392. [CrossRef]
* [PERSON] et al. (2020) [PERSON]; [PERSON]; [PERSON] Effect of pulsating injection and mainstream attack angle on film cooling performance of a gas turbine blade. _Phys. Fluids_**2020**, _32_, 117102. [CrossRef]
* [PERSON] et al. (2022) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] Effects of vortex generators and pulsation on compound angle film cooling. _Appl. Therm. Eng._**2022**, _244_, 122737. [CrossRef]
* [PERSON] et al. (2024) [PERSON]; [PERSON]; [PERSON]; [PERSON]; [PERSON] A conjugate study on the application of combined impingement and film cooling for a turbine blade tip. _Appl. Therm. Eng._**2024**, _252_, 123594.