[1] Huang Y., Yang V., Dynamics and stability of lean-premixed swirl-stabilized combustion. Progress in Energy and Combustion Science, 2009, 35(4): 293–364.
[2] Zhao D., Lu Z., Zhao H., et al., A review of active control approaches in stabilizing combustion systems in aerospace industry. Progress in Aerospace Sciences, 2018, 97: 35–60.
[3] Chen Y., Sun Y., Zhao D., Linear wave dynamics and intrinsic axisymmetric thermoacoustic instability in swirling flame combustors. Aerospace Science and Technology, 2021, 113: 106696.
[4] Li B., Shi B., Zhao X., et al., Oxy-fuel combustion of methane in a swirl tubular flame burner under various oxygen contents: Operation limits and combustion instability. Experimental Thermal and Fluid Science, 2018, 90: 115–124.
[5] Poinsot T., Prediction and control of combustion instabilities in real engines. Proceedings of the Combustion Institute, 2017, 36(1): 1–28.
[6] Moeck J.P., Durox D., Schuller T., et al., Nonlinear thermoacoustic mode synchronization in annular combustors. Proceedings of the Combustion Institute, 2019, 37(4): 5343–5350.
[7] Palies P., Durox D., Schuller T., et al., Nonlinear combustion instability analysis based on the flame describing function applied to turbulent premixed swirling flames. Combustion and Flame, 2011, 158(10): 1980–1991.
[8] Kabiraj L., Sujith R.I., Nonlinear self-excited thermoacoustic oscillations: intermittency and flame blowout. Journal of Fluid Mechanics, 2012, 713: 376–397.
[9] Yang D., Laera D., Morgans A.S., A systematic study of nonlinear coupling of thermoacoustic modes in annular combustors. Journal of Sound and Vibration, 2019, 456: 137–161.
[10] Song H., Lin Y., Han X., et al., The thermoacoustic instability in a stratified swirl burner and its passive control by using a slope confinement. Energy, 2020, 195: 116956.
[11] Zhao D., Ji C., Han N., et al., Experimental investigation of acoustic damping performance of double- and single-layer perforated liners: Effect of porosity and joint bias-grazing flow. 22nd AIAA/CEAS Aeroacoustics Conference, 2016.
[12] Zhao D., Gutmark E., Reinecke A., Mitigating self-excited flame pulsating and thermoacoustic os-cillations using perforated liners. Science Bulletin, 2019, 64(13): 941–952.
[13] Zhang G., Wang X., Li L., et al., Effects of perforated liners on controlling combustion instabilities in annular combustors. AIAA Journal, 2020, 58(7): 3100–3114.
[14] Zhao D., Li X.Y., A review of acoustic dampers applied to combustion chambers in aerospace industry. Progress in Aerospace Sciences, 2015, 74: 114–130.
[15] Karagozian A.R., The jet in crossflow. Physics of Fluids, 2014, 26(10): 101303.
[16] Li J., Huang J., Yan M., et al., Experimental study of n-heptane/air combustion in meso-scale burners with porous media. Experimental Thermal and Fluid Science, 2014, 52: 47–58.
[17] Zhou H., Tao C., Effects of annular N2/O2 and CO2/O2 jets on combustion instabilities and NOx emissions in lean-premixed methane flames. Fuel, 2020, 263: 116709.
[18] Murat Altay H., Hudgins D.E., Speth R.L., et al., Mitigation of thermoacoustic instability utilizing steady air injection near the flame anchoring zone. Combustion and Flame, 2010, 157(4): 686–700.
[19] LaBry Z.A., Shanbhogue S.J., Speth R.L., et al., Flow structures in a lean-premixed swirl-stabilized combustor with microjet air injection. Proceedings of the Combustion Institute, 2011, 33(1): 1575–1581.
[20] Uhm J.H., Acharya S., Control of combustion instability with a high-momentum air-jet. Combustion and Flame, 2004, 139(1–2): 106–125.
[21] Uhm J., Acharya S., Role of low-bandwidth open-loop control of combustion instability using a high-momentum air jet—mechanistic details. Combustion and Flame, 2006, 147(1–2): 22–31.
[22] Deshmukh N.N., Sharma S.D., Coefficient of Rayleigh Index based performance evaluation of radial microjet injection technique for thermoacoustic instability control. Measurement, 2020, 151: 107245.
[23] Oztarlik G., Selle L., Poinsot T., et al., Suppression of instabilities of swirled premixed flames with minimal secondary hydrogen injection. Combustion and Flame, 2020, 214: 266–276.
[24] Barbosa S., de La Cruz Garcia M., Ducruix S., et al., Control of combustion in-stabilities by local injection of hydrogen. Proceedings of the Combustion Institute, 2007, 31(2): 3207–3214.
[25] Ghoniem A.F., Annaswamy A., Park S., et al., Stability and emissions control using air injection and H2 addition in premixed combustion. Proceedings of the Combustion Institute, 2005, 30(2): 1765–1773.
[26] Rajpara P., Shah R., Banerjee J., Effect of hydrogen addition on combustion and emission char-acteristics of methane fuelled upward swirl can combustor. International Journal of Hydrogen Energy, 2018, 43(36): 17505–17519.
[27] Zhou H., Tang Q., Ren T., et al., Control of thermoacoustic instabilities by CO2 and N2 jet in cross-flow. Applied Thermal Engineering, 2012, 36: 353–359.
[28] Tao C., Zhou H., Effects of superheated steam on combustion instability and NOx emissions in a model lean premixed gas turbine combustor. Fuel, 2021, 288: 119646.
[29] Tao C., Zhou H., Dilution effects of CO2, Ar, N2 and He microjets on the combustion dynamic and emission characteristics of unsteady premixed flame. Aerospace Science and Technology, 2021, 111: 106537.
[30] Wang D., Ji C., Wang S., et al., Chemical effects of CO2 dilution on CH4 and H2 spherical flame. Energy, 2019, 185: 316–326.
[31] Lee K., Kim H., Park P., et al., CO2 radiation heat loss effects on NOx emissions and combustion instabilities in lean premixed flames. Fuel, 2013, 106: 682–689.
[32] Wei S., Yu M., Pei B., et al., Suppression of CO2 and H2O on the cellular instability of premixed methane/air flame. Fuel, 2020, 264(9): 116862.
[33] Gascoin N., Yang Q., Chetehouna K., Thermal effects of CO2 on the NOx formation behavior in the CH4 diffusion combustion system. Applied Thermal Engineering, 2017, 110: 144–149.
[34] Lee M.C., Seo S.B., Yoon J., et al., Experimental study on the effect of N2, CO2, and steam dilution on the combustion performance of H2 and CO synthetic gas in an industrial gas turbine. Fuel, 2012, 102: 431–438.
[35] Zhou H., Tao C., Liu Z., et al., Optimal control of turbulent premixed combustion instability with annular micropore air jets. Aerospace Science and Technology, 2020, 98: 105650.
[36] Tao C., Zhou H., Effects of different preheated CO2/O2 jet in cross-flow on combustion instabil-ity and emissions in a lean-premixed combustor. Journal of the Energy Institute, 2020, 93(6): 2334–2343.
[37] Deshmukh N.N., Sharma S.D., Suppression of thermoacoustic instability using air injection in horizontal Rijke tube. Journal of the Energy Institute, 2017, 90(3): 485–495.
[38] Xu Z., Zhang Y., Chen Y., Study on flow structure of tandem multiple jets under the effect of regular waves. Ocean Engineering, 2020, 217(3): 107993.
[39] Zhou M., Jiang H., Hu Y., et al., The formation of steady gas film on the inner wall of the radial multiple jets-in-crossflow reactor. Chemical Engineering and Processing-Process Intensification, 2019, 143: 107617.
[40] Chen J., Li J., Yuan L., et al., Flow and flame characteristics of a RP-3 fuelled high temperature rise combustor based on RQL. Fuel, 2019, 235: 1159–1171.
[41] Liu R., Zhou Z., Xiao R., et al., CFD-DEM modelling of mixing of granular materials in multiple jets fluidized beds. Powder Technology, 2020, 361: 315–325.
[42] Kannan B.T., Panchapakesan N.R., Influence of nozzle configuration on the flow field of multiple jets. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 232(9): 1639–1654.
[43] Kamal M.M., Development of a multiple opposing jets’ burner for premixed flames. Proceed-ings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2012, 226(8): 1032–1049.
[44] Zhou M., Jiang H., Hu Y., et al., Evaluation of mixing performance for the industrial-scale radial multiple jets-in-crossflow mixing structure. Chemical Engineering and Processing-Process Intensification, 2019, 141: 107534.
[45] Doerr T., Blomeyer M., Hennecke D.K., Optimization of multiple jets mixing with a confined cross-flow. Journal of Engineering for Gas Turbines and Power-Transactions of the ASME, 1997, 119(2): 315–321.
[46] Thong C.X., Dally B.B., Birzer C.H., et al., An experimental study on the near flow field of a round jet affected by upstream multi-lateral side-jet. Experimental Thermal and Fluid Science, 2017, 82: 198–211.
[47] Menon R., Gollahalli S.R., Combustion characteristics of interacting multiple jets in cross flow. Combustion Science and Technology, 1988, 60(4–6): 375–389.
[48] Zhou H., Hu L.B., Mitigation of combustion instability and NOx emissions by microjets in lean premixed flames with different swirl numbers. Journal of Thermal Science, 2023, 32(4): 1697–1709.
[49] Wachsman A., Park S., Annaswamy A., et al., Simultaneous combustion instability and emissions control using air and fuel modulation. 42nd AIAA Aerospace Sci-ences Meeting and Exhibit, 2004.
[50] Mahesh K., The interaction of jets with crossflow. Annual Review of Fluid Mechanics, 2013, 45(1): 379–407.
[51] Sun Y., Sun M., Zhu J., et al., PLIF measurements of instantaneous flame structures and curvature of an acoustically excited turbulent premixed flame. Aerospace Science and Technology, 2020, 104: 105950.
