[1] Lefebvre A., Gas turbine combustion: alternative fuels and emissions. CRC Press, New York, 2010.
[2] Langston L.S., Crossflows in a turbine cascade passage. Journal of Engineering for Power, 1980, 102(4): 866–874.
[3] Sharma J.P., Butler T.L., Predictions of endwall losses and secondary flows in axial flow turbine cascades. ASME Journal of Turbomachinery, 1987, 109(2): 229–236.
[4] Wang H.P., Olson S.J., Goldstein R.J., Eckert E.R.G., Flow visualization in a linear turbine cascade of high performance turbine blades. ASME Journal of Turbomachinery, 1997, 119(1): 1–8.
[5] Pu J., Yu J., Wang J.H., Yang W.S., Zhang Z.Q., Wang L., An experimental investigation of secondary flow characteristics in a linear turbine cascade with upstream converging slot-holes using TR-PIV. Experimental Thermal and Fluid Science, 2014, 59: 56–71.
[6] Knost D.G., Thole K.A., Adiabatic effectiveness measurements of endwall film cooling for a first stage vane. ASME Journal of Turbomachinery, 2005, 127(2): 297–305.
[7] Li X.Y., Ren J., Jiang H.D., Influence of different film cooling arrangements on endwall cooling. International Journal of Heat and Mass Transfer, 2016, 102: 348–359.
[8] Francesca S., Giovanni T., Effect of discrete-hole arrangement on film-cooling effectiveness for the endwall of a turbine blade cascade. Applied Thermal Engineering, 2015, 91: 507–514.
[9] Wang X., Xu H.Z., Wang J.H., Song W., Wang M., Multi-objective optimization of discrete film hole arrangement on a high pressure turbine endwall with conjugate heat transfer simulations. International Journal of Heat and Fluid Flow, 2019, 78: 108428.
[10] Zhang J., Liu C.L., Zhang L., Zhou T.L., Li L., Guo Y.H., Experimental study of film cooling characteristics of annular cascade endwall with a partitioned film cooling layout. International Journal of Thermal Sciences, 2022, 182: 107821.
[11] Friedrichs S., Hodson H.P., Dawes W.N., Aerodynamic aspects of endwall film-cooling. ASME Journal of Turbomachinery, 1997, 119(4): 786–793.
[12] Mensch A.E., Thole K.A., Effects of non‑axisymmetric endwall contouring and film cooling on the passage flowfield in a linear turbine cascade. Experiments in Fluids, 2016, 57(1): 1.
[13] Ghopa W.A.W., Harun Z., Funazaki K., Miura T., Aero-thermal performances of leakage flow injection from the endwall slot in a linear cascade of high-pressure turbine. Journal of Thermal Science, 2015, 24(1): 49–57.
[14] Zhang L.Z., Hee K.M., Turbine nozzle endwall inlet film cooling the effect of a back-facing step. ASME, GT2003-38319.
DOI: https://doi.org/10.1115/GT2003-38319
[15] Xiao X.T., Wang P., Du Q., Xu Q.Z., Liu J., Zhu J.Q., Numerical investigations of film cooling characteristics of interrupted slot and trench holes on a vane endwall. Journal of Thermal Science, 2021, 30(3): 1010–1024.
[16] Bai B., Li Z.G., Li J., et al., Effects of upstream step geometry on axisymmetric converging vane endwall heat transfer and film cooling at transonic conditions. ASME, GT2020-16154.
DOI: 10.1115/GT2020-16154
[17] Luke L., Ridge S., Shuo M., et al., The effect of step misalignment on purge flow cooling of nozzle guide vane at transonic conditions. ASME Journal of Turbomachinery, 2020, 142(10): 101004.
[18] Gunther M., Christian L., Martin B., Robert K., Turbine vane endwall film cooling effectiveness of different purge slot configurations in a linear cascade. ASME Journal of Turbomachinery, 2020, 142(3): 031008.
[19] Zhang Y., Yuan X., Turbine endwall film cooling with combustor-turbine interface gap leakage flow: effect of incidence angle. Journal of Thermal Science, 2013, 22(2): 135−144.
[20] Yao Y.J., Zhu P.Y., Tao Z., Song L.M., Li J., Experimental study on the effects of slot jet on film cooling performance in the cascade endwall with purge flow. ASME, GT2019-90667.
DOI: https://doi.org/10.1115/GT2019-90667
[21] Thrift A.A., Thole K.A., Hada S., Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall. ASME Journal of Turbomachinery, 2012, 134(6): 061019.
[22] Tao Z., Yao Y.J., Zhu P.Y., Song L.M., Li J., Experimental and numerical study on film cooling effectiveness of an annular cascade endwall with different slot configuration. International Journal of Thermal Sciences, 2020, 158: 106517.
[23] Thrift A.A., Thole K.A., Influence of flow injection angle on a leading-edge horseshoe vortex. International Journal of Heat and Mass Transfer, 2012, 55(17): 4651–4664.
[24] Kim J.J., Sohn H.S., Choi S.Y, et al., Effect of misalignment at 2nd vane endwall on heat transfer with purge flow. International Journal of Heat and Mass Transfer, 2021, 170: 121034.
[25] Xu Q.Z., Du Q., Wang P., Liu J., Liu G., Computational investigation of film cooling and secondary flow on turbine endwall with coolant injection from the upstream interrupted slot. International Journal of Heat and Mass Transfer, 2018, 123: 285–296.
[26] Ye L., Liu C.L., Du K., Chen L., Wang Y.M., Zhu A.D., Influences of groove configuration and density ratio on grooved leading-edge showerhead film cooling using the pressure sensitive paint measurement technique. International Journal of Heat and Mass Transfer, 2022, 190: 122641.
[27] Ye L., Liu C.L., Zhu A.D., Zhang F., Zhang C.X., Cooling characteristics of the trailing-edge slot downstream from internal multi-ribbed channel. International Journal of Heat and Mass Transfer, 2022, 183: 122057.
[28] Zhang B.L., Yao C.Y., Zhu H.R., Liu C.L., Stunden B., Experimental study on film cooling performance of a turbine blade tip with a trapezoidal slot cooling scheme in transonic flow using PSP technique. Experimental Thermal and Fluid Science, 2022, 130: 110513.
[29] Kline S.J., McClintock, F.A., Describing uncertainties in single-sample experiments. Mechanical Engineering, 1953, 75: 3–8.
[30] Robert J.M., Describing the uncertainties in experimental results. Experimental Thermal and Fluid Science, 1988, 1(1): 3–17.
[31] Thrift A.A., Thole K.A., Hada S., Effects of an axisymmetric contoured endwall on a nozzle guide vane: convective heat transfer measurements. ASME Journal of Turbomachinery, 2011, 133(4): 041008.