[1] Ye L., Liu C.L., Zhu H.R., Luo J.X., Experimental investigations on the effect of cross-flow Reynolds number on film cooling effectiveness. AIAA Journal, 2019, 57(11): 4804–4818.
[2] Bunker R.S., Film cooling: Breaking the limits of diffusion shaped holes. Heat Transfer Research, 2010, 41(1): 627–650.
[3] Liu, C.L., Li, B.R., Song, H., Chen, L., Wang, R., Wang, Y.M., Liang, D.P., Study on effects of spanwise-expansion parameters on film cooling effectiveness of diffusion shaped hole configurations. Journal of Turbomachinery, 2023, 145(1): 011003.
[4] Zhu H., Tao G., Xu D.C., Investigation of film cooling and superposition method for double row dustpan-shaped holes. Heat Transfer—Asian Research, 2010, 37(4): 208–217.
[5] Zhai Y.N., Liu C.L., He Y.H., Zhou Z.X., Investigation on the film cooling performance of diffuser shaped holes with different inclination angles. International Journal of Turbo & Jet-Engines, 2017, 34(2): 123–139.
[6] Ye L., Liu C.L., Xu Z.P., Zhu H.R., Liu H.Y., Zhai Y.-N., Experimental investigation on the adiabatic film effectiveness for counter-inclined simple and laid-back film-holes of leading edge. Journal of Thermal Science, 2020, 29(3): 772–783.
[7] Chin J.H., Skirvin S.C., Hayes L.E., Burggraf F., Film cooling with multiple slots and louvers. Journal of Heat Transfer, 1961, 83(3): 281–291.
[8] Sellers J.P., Gaseous film cooling with multiple injection stations. AIAA Journal, 1963, 1(9): 2154–2156.
[9] Sasaki M., Takahara K., Kumagai T., Hamano M., Film cooling effectiveness for injection from multirow holes. ASME Journal of Engineering Power, 1979, 101(1): 101–108.
[10] Harrington M.K., Mcwaters M.A., Bogard D.G., Lemmon C.A., Thole K.A., Full-coverage film cooling with short normal injection holes. Journal of Turbomachinery, 2001, 123(4): 798–805.
[11] Saumweber C., Schulz A., Interaction of film cooling rows: Effects of hole geometry and row spacing on the cooling performance downstream of the second row of holes. Journal of Turbomachinery, 2004, 126(2): 237– 246.
[12] Meng T., Zhu H.R., Liu C.L., Wei J.S., Investigation on the accuracy of superposition predictions of film cooling effectiveness. International Journal of Turbo & Jet-Engines, 2018, 35(2): 181–192.
[13] Wang L., Li X.Y., Ren J., Jiang H.D., Effect of row spacing on the accuracy of film cooling superposition method. ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, 2018, Volume 5C: Heat Transfer, Paper No: GT2018-76421, V05CT19A025. DOI: 10.1115/GT2018-76421.
[14] Meng T., Zhu H.R., Liu C.L., Xu B.H., Superposition prediction accuracy of film cooling efficiency on turbine blade. Journal of Xi’an Jiaotong University, 2018, 52(4): 55–62. (in Chinese)
[15] Mhetras S., Han J.-C., Effect of superposition on spanwise film-cooling effectiveness distribution on a gas turbine blade. ASME International Mechanical Engineering Congress and Exposition, 2006, Paper No: IMECE2006-15084, pp. 477–487. DOI: 10.1115/IMECE2006-15084.
[16] Luckey D.W., Lecuyer M.R., Stagnation region gas film cooling: Spanwise angled injection from multiple rows of holes. 1981, NASA-CR-165333.
[17] Anderson J.B., Winka J.R., Bogard D.G., Crawford M.E., Evaluation of superposition predictions for showerhead film cooling on a vane. Journal of Turbomachinery, 2015, 137(4): 041010.
[18] Andreini A., Carcasci C., Gori S., Surace M., Film cooling system numerical design: Adiabatic and conjugate analysis. ASME Summer Heat Transfer Conference, 2005, Paper No: HT2005-72042, pp. 9–20. DOI: 10.1115/HT2005-72042.
[19] Cutbirth J.M., Bogard D.G., Evaluation of pressure side film cooling with flow and thermal field measurements - Part II: Turbulence effects. Journal of Turbomachinery, 2002, 124(4): 678–685.
[20] Kinell M., Utriainen E., Najafabadi H.N., Karlsson M., Barabas B., Comparison of gas turbine vane pressure side and suction side film cooling performance and the applicability of superposition. ASME Turbo Expo: Turbine Technical Conference & Exposition. 2012, Paper No: GT2012-68994, pp. 1479–1489. DOI: 10.1115/GT2012-68994.
[21] Zhang F., Liu C.L., Ye L., Li B.R., Zhang S.Q., Experimental investigation on cooling performance of impingement-effusion full coverage film on suction surface of a vane. Journal of Turbomachinery, 2021, 143(12): 121007.
[22] Schnieder M., Parneix S., Von Wolfersdorf J., Effect of showerhead injection on superposition of multirow pressure side film cooling with fan shaped holes. ASME Turbo Expo, 2003, Paper No: GT2003-38693, pp. 559–568. DOI: 10.1115/GT2003-38693.
[23] Grives E. Le, Nicolas J.J., Genot J., Internal aerodynamics and heat transfer problems associated to film cooling of gas turbines. American Society of Mechanical Engineers (Paper), 1979, Paper No: 79-GT-57, V01AT01A057. DOI: 10.1115/79-GT-57.
[24] Kirollos B., Povey T., An energy-based method for predicting the additive effect of multiple film cooling rows. Journal of Engineering for Gas Turbines and Power, 2015, 137(12): 122607.
[25] Zhu H.R., Guo T., Xu D.C., Film cooling and superposition method for double row dust-pan shaped holes. Journal of Aerospace Power, 2006, 21(5): 814–819.(in Chinese)
[26] Ye L., Liu C.L., Zhou D.E., Zhu H.R., Experimental and numerical investigations on the heat transfer of film-cooling with cylindrical holes fed with internal coolant cross flows. Journal of Heat Transfer, 2020, 142(5): 052302.
[27] Bai J.L., Zhu H.R., Liu C.L., Analysis of uncertainties in two-parameter transient heat transfer measurements with liquid crystal. Journal of Aerospace Power, 2009, 24(9): 1945–1951. (in Chinese)
[28] Moffat R.J., Describing the uncertainties in experimental results. Experimental Thermal and Fluid Science, 1988, 1(1): 3–17.
[29] Lynch S.P., Thole K.A., Kohli A., Lehane C., Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring. Journal of Turbomachinery, 2011, 133(4): 041003.
[30] Lee K.D., Kim K.Y., Numerical study on film-cooling performance of a novel shaped hole. International Symposium on Fluid Machinery and Fluids Engineering, 2012, Paper No: GT2012-68529, pp. 1345–1355.
DOI: 10.1115/GT2012-68529.
[31] Ekkad S.V., Mehendale A.B, Han J.C., Combined effect of grid turbulence and unsteady wake on film effectiveness and heat transfer coefficient of a gas turbine blade with air and CO2 film injection. Journal of Turbomachinery, 1997, 119(3): 594–600.
[32] Yu Y., Yen C.-H., Shih T.I.-P., Film cooling effectiveness and heat transfer coefficient distributions around diffusion shaped holes. Journal of Heat Transfer, 2002, 124(5): 820–827.