[1] S.-H. Lee, Characteristics of dual transverse injection in scramjet combustor, part 1: mixing, J. Propul. Power 22 (2006) 1012–1019.
[2] L. Li, W. Huang, L. Yan, S. Li, Parametric effect on the mixing of the combination of a hydrogen porthole with an air porthole in transverse gaseous injection flow fields, Acta Astronaut. 139 (2017) 435–448.
[3] E.T. Curran, Scramjet engines: the first forty years, J. Propul. Power 17 (2001) 1138–1148. https://doi.org/10.2514/2.5875.
[4] F. Ladeinde, A critical review of scramjet combustion simulation, in: 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2009: p. 127.
[5] C. Segal, The scramjet engine: processes and characteristics, Cambridge University Press, 2009.
[6] Z. Xiang, X. Zhixun, M. Likun, L. Chaolong, F. Chuanbo, G. Alon, Others, Research progress on solid-fueled scramjet, Chin. J. Aeronaut. 35 (2022) 398–415.
[7] D.W. Bogdanoff, Advanced injection and mixing techniques for scramjet combustors, J. Propul. Power 10 (1994) 183–190.
[8] M.B. Gerdroodbary, Scramjets: fuel mixing and injection systems, Butterworth-Heinemann, 2020.
[9] Q. Guan, J. Liang, M. Sun, L. Zhang, W. Chen, Large eddy simulation of supersonic mixing layers using a compressible filtered mass density function method, Aerospace Science and Technology 124 (2022) 107425. https://doi.org/10.1016/j.ast.2022.107425.
[10] K. Jin, X. Cai, R. Hong, L. Zhang, J. Liang, Numerical investigation on flow choking induced by local heat release and large-scale flow separation in a supersonic combustor, Combustion and Flame 268 (2024) 113627. https://doi.org/10.1016/j.combustflame.2024.113627.
[11] W. Waidmann, F. Alff, M. B?hm, U. Brummund, W. Clauss, M. Oschwald, Supersonic combustion of hydrogen/air in a scramjet combustion chamber, Space Technol. 15 (1996) 421–429.
[12] F. Génin, S. Menon, Simulation of turbulent mixing behind a strut injector in supersonic flow, AIAA J. 48 (2010) 526–539.
[13] P. Manna, R. Behera, D. Chakraborty, Liquid-fueled strut-based scramjet combustor design: a computational fluid dynamics approach, J. Propul. Power 24 (2008) 274–281.
[14] W. Huang, Investigation on the effect of strut configurations and locations on the combustion performance of a typical scramjet combustor, J. Mech. Sci. Technol. 29 (2015) 5485–5496.
[15] R.K. Soni, A. De, Investigation of strut-ramp injector in a scramjet combustor: effect of strut geometry, fuel and jet diameter on mixing characteristics, J. Mech. Sci. Technol. 31 (2017) 1169–1179.
[16] L. Li, W. Huang, L. Yan, Z. Du, M. Fang, Numerical investigation and optimization on the micro-ramp vortex generator within scramjet combustors with the transverse hydrogen jet, Aerosp. Sci. Technol. 84 (2019) 570–584. https://doi.org/10.1016/j.ast.2018.11.011.
[17] J. Zhang, S. Dou, X. Wang, M. Li, Q. Yang, X. Xu, Investigation on combustor performance of a ramp-based solid rocket scramjet with ethylene addition, Acta Astronaut. (2025).
[18] S.P. Jeyakumar, A.S. Patale, P. Sharma, Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor, Int. J. Turbo Jet Engines 41 (2024) 449–462.
[19] J. Moorthy, B. Rajinikanth, B. Charyulu, G.A.P. Rao, Effect of ramp-cavity on hydrogen fueled scramjet combustor, Propul. Power Res. 3 (2014) 22–28.
[20] J.L. Ruan, P. Domingo, G. Ribert, Analysis of combustion modes in a cavity based scramjet, Combust. Flame 215 (2020) 238–251. https://doi.org/10.1016/j.combustflame.2020.01.034.
[21] Q. Liu, D. Baccarella, W. Landsberg, A. Veeraragavan, T. Lee, Cavity flameholding in an optical axisymmetric scramjet in mach 4.5 flows, Proc. Combust. Inst. 37 (2019) 3733–3740.
[22] Y. Meng, H. Gu, J. Zhuang, W. Sun, Z. Gao, H. Lian, L. Yue, X. Chang, Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration, Aerosp. Sci. Technol. 93 (2019) 105316.
[23] L. Mingjiang, S. Mingbo, Y. Daoning, Z. Guoyan, T. Tao, A. Bin, W. Hongbo, Mixing and combustion characteristics in a scramjet combustor with different distances between cavity and backward-facing step, Chin. J. Aeronaut. 36 (2023) 400–411.
[24] X. Zhang, L. Yue, T. Huang, Q. Zhang, X. Zhang, Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor, Aerosp. Sci. Technol. 94 (2019) 105420.
[25] X. Pei, L. Hou, Numerical investigation on cavity structure of solid-fuel scramjet combustor, Acta Astronaut. 105 (2014) 463–475.
[26] L. Suneetha, P. Randive, K. Pandey, Numerical investigation on implication of dual cavity on combustion characteristics in strut based scramjet combustor, Int. J. Hydrogen Energy 44 (2019) 32080–32094.
[27] J. Tishkoff, J. Drummond, T. Edwards, A. Nejad, J. Tishkoff, J. Drummond, T. Edwards, A. Nejad, Future directions of supersonic combustion research-air force/NASA workshop on supersonic combustion, in: 35th Aerospace Sciences Meeting and Exhibit, 1997: p. 1017.
[28] J. Urzay, Supersonic combustion in air-breathing propulsion systems for hypersonic flight, Annu. Rev. Fluid Mech. 50 (2018) 593–627.
[29] L. Zhang, J. Liang, M. Sun, H. Wang, Experimental investigation of combustion stabilization modes in a cavity-based supersonic combustor with different wall divergence angles, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232 (2018) 1853–1863. https://doi.org/10.1177/0954410017710270.
[30] L. Zhang, Y. Cao, J. Liang, Y. Wang, M. Sun, Effects of inflow velocity on transverse jet injection in a supersonic cavity combustor, Physics of Fluids 35 (2023) 116121. https://doi.org/10.1063/5.0177228.
[31] J. Li, J. Liang, M. Sun, Z. Cai, L. Zhang, Combustion enhancement subjected to the inlet distortion in a cavity-based supersonic combustor, Aerospace Science and Technology 142 (2023) 108636. https://doi.org/10.1016/j.ast.2023.108636.
[32] S. Lawson, G.N. Barakos, Review of numerical simulations for high-speed, turbulent cavity flows, Prog. Aerosp. Sci. 47 (2011) 186–216.
[33] Z. Wang, H. Wang, M. Sun, Review of cavity-stabilized combustion for scramjet applications, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 228 (2014) 2718–2735. https://doi.org/10.1177/0954410014521172.
[34] F.W. Barnes, C. Segal, Cavity-based flameholding for chemically-reacting supersonic flows, Progress in Aerospace Sciences 76 (2015) 24–41. https://doi.org/10.1016/j.paerosci.2015.04.002.
[35] W. Huang, Mixing enhancement strategies and their mechanisms in supersonic flows: a brief review, Acta Astronaut. 145 (2018) 492–500. https://doi.org/10.1016/j.actaastro.2018.02.022.
[36] Z. Cai, T. Wang, M. Sun, Review of cavity ignition in supersonic flows, Acta Astronautica 165 (2019) 268–286. https://doi.org/10.1016/j.actaastro.2019.09.016.
[37] M. Ding, Research on supersonic combustion flame stabilization based on cavity, Doctoral dissertation, National University of Defense Technology, 2005.
[38] V.A. Vinogradov, S.A. Kobigsky, M.D. Petrov, Experimental investigation of kerosene fuel combustion in supersonic flow, J. Propul. Power 11 (1995) 130–134.
[39] R. Milligan, J. Liu, C.-J. Tam, D. Eklund, M. Gruber, D. Davis, D. Risha, M. Gruber, T. Mathur, Dual-mode scramjet combustor: numerical sensitivity and evaluation of experiments, in: 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2012: p. 947.
[40] R. Milligan, D. Eklund, J. Wolff, T. Mathur, M. Gruber, Dual mode scramjet combustor: analysis of two configurations, in: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2010: p. 751.
[41] R.L. Stallings Jr, F.J. Wilcox Jr, Experimental cavity pressure distributions at supersonic speeds, 1987.
[42] W. Li, T. Nonomura, A. Oyama, K. Fujii, LES study of feedback-loop mechanism of supersonic open cavity flows, in: 40th Fluid Dynamics Conference and Exhibit, 2010: p. 5112.
[43] T. Colonius, An overview of simulation, modeling, and active control of flow/acoustic resonance in open cavities, in: 39th Aerospace Sciences Meeting and Exhibit, 2001: p. 76.
[44] D.L. Davis, Numerical analysis of two and three dimensional recessed flame holders for scramjet applications, Air Force Institute of Technology, 1996.
[45] R. Baurle, C.-J. Tam, S. Dasgupta, Analysis of unsteady cavity flows for scramjet applications, in: 35th Intersociety Energy Conversion Engineering Conference and Exhibit, 2000.
[46] R. Baurle, C.-J. Tam, J. Edwards, H. Hassan, Hybrid simulation approach for cavity flows: blending, algorithm, and boundary treatment issues, AIAA J. 41 (2003) 1463–1480.
[47] W. Wang, M. He, B. Yu, X. Han, Y. Ji, Z. Yin, X. Huang, H. Liu, On the residence enhancement mechanism of the cavity-based dual-mode scramjet combustor through the eulerian and lagrangian analysis, Physics of Fluids 36 (2024) 026103. https://doi.org/10.1063/5.0183825.
[48] C. Liu, Y. Zhao, Z. Wang, H. Wang, M. Sun, Dynamics and mixing mechanism of transverse jet injection into a supersonic combustor with cavity flameholder, Acta Astronaut. 136 (2017) 90–100. https://doi.org/10.1016/j.actaastro.2017.03.010.
[49] C. Liu, Z. Wang, M. Sun, H. Wang, P. Li, Characteristics of a cavity-stabilized hydrogen jet flame in a model scramjet combustor, AIAA Journal 57 (2019) 1624–1635. https://doi.org/10.2514/1.J057346.
[50] N. Sato, A. Imamura, S. Shiba, S. Takahashi, M. Tsue, M. Kono, Advanced mixing control in supersonic airstream with a wall-mounted cavity, J. Propul. Power 15 (1999) 358–360.
[51] W. Huang, Z. Du, L. Yan, R. Moradi, Flame propagation and stabilization in dual-mode scramjet combustors: a survey, Prog. Aerosp. Sci. 101 (2018) 13–30.
[52] T. Kitagawa, A. Moriwaki, K. Murakami, K. Takita, G. Masuya, Ignition characteristics of methane and hydrogen using a plasma torch in supersonic flow, J. Propul. Power 19 (2003) 853–858.
[53] H. Do, M.A. Cappelli, M.G. Mungal, Plasma assisted cavity flame ignition in supersonic flows, Combust. Flame 157 (2010) 1783–1794.
[54] S. Brieschenk, S. O’Byrne, H. Kleine, Ignition characteristics of laser-ionized fuel injected into a hypersonic crossflow, Combust. Flame 161 (2014) 1015–1025.
[55] T.M. Ombrello, C.D. Carter, C.-J. Tam, K.-Y. Hsu, Cavity ignition in supersonic flow by spark discharge and pulse detonation, Proc. Combust. Inst. 35 (2015) 2101–2108.
[56] Y. Wang, W. Song, Experimental investigation of influence factors on flame holding in a supersonic combustor, Aerosp. Sci. Technol. 85 (2019) 180–186.
[57] M.A. Goldfeld, Y.V. Zakharova, A.V. Fedorov, N.N. Fedorova, Effect of the wave structure of the flow in a supersonic combustor on ignition and flame stabilization, Combust. Explos. Shock Waves 54 (2018) 629–641.
[58] B. An, L. Yang, Z. Wang, X. Li, M. Sun, J. Zhu, W. Yan, Characteristics of laser ignition and spark discharge ignition in a cavity-based supersonic combustor, Combust. Flame 212 (2020) 177–188.
[59] D.J. Micka, J.F. Driscoll, Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder, Proceedings of the Combustion Institute 32 (2009) 2397–2404. https://doi.org/10.1016/j.proci.2008.06.192.
[60] H. Wang, Z. Wang, M. Sun, H. Wu, Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor, International Journal of Hydrogen Energy 38 (2013) 12078–12089. https://doi.org/10.1016/j.ijhydene.2013.06.132.
[61] Y.-X. Zhang, Z.-G. Wang, M.-B. Sun, Y.-X. Yang, H.-B. Wang, Hydrogen jet combustion in a scramjet combustor with the rearwall-expansion cavity, Acta Astronautica 144 (2018) 181–192. https://doi.org/10.1016/j.actaastro.2017.12.029.
[62] Y. Yang, Study on supersonic flow patterns and flame stabilization mechanism of trailing-edge expanded cavity, Doctoral dissertation, National University of Defense Technology, 2018.
[63] M. Gharib, A. Roshko, The effect of flow oscillations on cavity drag, J. Fluid Mech. 177 (1987) 501–530.
[64] C.W. Rowley, A.J. BASU<sup>, On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities, J. Fluid Mech. (2002) 315–346.
[65] E. Curran, S. Murthy, High-speed flight systems, 1991, vol. 137, Doi 10 (n.d.) 21–100.
[66] G. Ma, M. Sun, F. Li, Y. Yang, Y. Huang, H. Wang, Effect of fuel injection distance and cavity depth on the mixing and combustion characteristics of a scramjet combustor with a rear-wall-expansion cavity, Acta Astronautica 182 (2021) 432–445. https://doi.org/10.1016/j.actaastro.2021.02.020.
[67] Z. Ren, B. Wang, B. Hu, L. Zheng, Numerical analysis of supersonic flows over an aft-ramped open-mode cavity, Aerospace Science and Technology 78 (2018) 427–437. https://doi.org/10.1016/j.ast.2018.05.003.
[68] N. Zhuang, F.S. Alvi, M.B. Alkislar, C. Shih, Supersonic cavity flows and their control, Am. Inst. Aeronaut. Astronaut. (2006) 2118–2128.
[69] Z.H. C. Wang Z. Jiang, J. Lu, Numerical investigation on the flowfield of “swallowtail-cavity for supersonic mixing enhancement, Acta Mech. Sin. (2009) 37–44.
[70] H. Wang, M. Sun, N. Qin, H. Wu, Z. Wang, Characteristics of oscillations in supersonic open cavity flows, Flow Turbul. Combust. 90 (2013) 121–142.
[71] N. Zhuang, F. Alvi, C. Shih, Another look at supersonic cavity flows and their control, in: 11th AIAA/CEAS Aeroacoustics Conference, 2005: p. 2803.
[72] K.A. Lad, R.R. Vinil Kumar, A. Vaidyanathan, Experimental study of subcavity in supersonic cavity flow, AIAA Journal 56 (2018) 1965–1977. https://doi.org/10.2514/1.J056361.
[73] M.R. Gruber, R.A. Baurle, T. Mathur, Fundamental studies of cavity-based flameholder concepts for supersonic combustors, (n.d.).
[74] N. Relangi, D. Garimella, K. Jayaraman, J. Venkatesan, S. Jeyakumar, A. Ingenito, Others, Numerical simulations of axisymmetric aft wall angle cavity in supersonic combustion ramjets, Proc. AIAA Propuls Energy (2020) 1–15.
[75] S. Jeyakumar, S.M. Assis, K. Jayaraman, Effect of axisymmetric aft wall angle cavity in supersonic flow field, Int. J. Turbo Jet Engines 35 (2018) 29–34.
[76] R. Baurle, M. Gruber, A study of recessed cavity flowfields for supersonic combustion applications, in: 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998: p. 938.
[77] K. Kannaiyan, Computational study of the effect of cavity geometry on the supersonic mixing and combustion of ethylene, J. Comput. Sci. 47 (2020) 101243. https://doi.org/10.1016/j.jocs.2020.101243.
[78] W. Du, B. Wu, Numerical study of supersonic combustion with cavities of different lengths, Rocket Propuls. 31 (2005) 26–29.
[79] Z. Jia, D. Wu, Y. Pu, M. Xue, Effect of cavity leading edge angle on supersonic combustion chamber performance, J. Aerosp. Power 27 (2012) 993–998.
[80] N.K. Mahto, G. Choubey, L. Suneetha, K. Pandey, Effect of variation of length-to-depth ratio and mach number on the performance of a typical double cavity scramjet combustor, Acta Astronaut. 128 (2016) 540–550.
[81] F. Li, M. Sun, Z. Cai, Y. Sun, F. Li, J. Zhang, J. Zhu, Experimental study of flame stabilization in a single-side expansion scramjet combustor with different cavity length-to-depth ratios, Acta Astronautica 173 (2020) 1–8. https://doi.org/10.1016/j.actaastro.2020.03.034.
[82] Y. Prokesch, A. Duran, D. Gallegos, E. Schlussel, G. Young, Effect of flameholding cavity geometry on the flowfield of a solid fuel scramjet, Acta Astronaut. 224 (2024) 508–519. https://doi.org/10.1016/j.actaastro.2024.08.036.
[83] J. Yu, Z. Zhou, J. Peng, T. Tang, W. Yang, Y. Yang, H. Wang, Optimization design of scramjet combustor configuration parameters based on surrogate model, Chin. J. Theor. Appl. Mech. 56 (2024) 1–12.
[84] R. Moradi, A. Mahyari, M. Barzegar Gerdroodbary, A. Abdollahi, Y. Amini, Shape effect of cavity flameholder on mixing zone of hydrogen jet at supersonic flow, Int. J. Hydrogen Energy 43 (2018) 16364–16372. https://doi.org/10.1016/j.ijhydene.2018.06.166.
[85] O.R. Kummitha, K.M. Pandey, R. Gupta, CFD analysis of a scramjet combustor with cavity based flame holders, Acta Astronaut. 144 (2018) 244–253. https://doi.org/10.1016/j.actaastro.2018.01.005.
[86] O.R. Kummitha, K.M. Pandey, R. Gupta, Optimization of scramjet performance with different fuel injection techniques and flame holder cavities, Acta Astronautica 152 (2018) 908–919. https://doi.org/10.1016/j.actaastro.2018.09.026.
[87] S. Luo, W. Huang, J. Liu, Z. Wang, Drag force investigation of cavities with different geometric configurations in supersonic flow, Sci. China Technol. Sci. 54 (2011) 1345–1350. https://doi.org/10.1007/s11431-011-4320-5.
[88] Y. Jiang, A. Poozesh, S.M. Marashi, R. Moradi, M. Barzegar Gerdroodbary, A. Shafee, Z. Li, H. Babazadeh, Effect of cavity back height on mixing efficiency of hydrogen multi-jets at supersonic combustion chamber, International Journal of Hydrogen Energy 45 (2020) 27828–27836. https://doi.org/10.1016/j.ijhydene.2020.07.001.
[89] Z. Cai, M. Sun, Z. Wang, X.-S. Bai, Effect of cavity geometry on fuel transport and mixing processes in a scramjet combustor, Aerospace Science and Technology 80 (2018) 309–314. https://doi.org/10.1016/j.ast.2018.07.028.
[90] Z. Cai, X. Liu, C. Gong, M. Sun, Z. Wang, X.-S. Bai, Large eddy simulation of the fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity, Acta Astronaut. 126 (2016) 375–381.
[91] J. Li, J. Liang, Z. Cai, M. Sun, L. Zhang, Experimental study on the flame stabilization mode in the rear-wall-expansion cavity, Aerospace Science and Technology 130 (2022) 107859. https://doi.org/10.1016/j.ast.2022.107859.
[92] W.O. Landsberg, D. Curran, A. Veeraragavan, Experimental flameholding performance of a scramjet cavity with an inclined front wall, Aerospace Science and Technology 126 (2022) 107622. https://doi.org/10.1016/j.ast.2022.107622.
[93] T.V. Krishna, P. Kumar, S. Das, S.L.N. Desikan, Effect of cavity rear wall modifications on pressure fluctuations at supersonic speed, Acta Astronautica 185 (2021) 78–88. https://doi.org/10.1016/j.actaastro.2021.04.030.
[94] V. Kumar, K.M. Pandey, Recent advances in development of supersonic efficient combustors, Materials Today: Proceedings 45 (2021) 6889–6894. https://doi.org/10.1016/j.matpr.2020.12.1092.
[95] A. Oamjee, R. Sadanandan, Fuel injection location studies on pylon-cavity aided jet in supersonic crossflow, Aerosp. Sci. Technol. 92 (2019) 869–880.
[96] A. Oamjee, R. Sadanandan, Effects of fuel injection angle on mixing performance of scramjet pylon-cavity flameholder, Physics of Fluids 32 (2020) 116108. https://doi.org/10.1063/5.0026125.
[97] Z. Qiuru, Y. Huanli, D. Jian, Effects of cavity-induced mixing enhancement under oblique shock wave interference: numerical study, Int. J. Hydrogen Energy 46 (2021) 35706–35717.
[98] D. Jian, Z. Qiuru, Numerical investigation on mixing enhancement of the cavity with pulsed jets under oblique shock wave interference, Aerosp. Sci. Technol. 123 (2022) 107454.
[99] Z. Du, C. Shen, W. Huang, Y. Han, Investigation on the impact of the induced shock wave on the hydrogen mixing augmentation in a supersonic crossflow: a numerical study, Fuel 312 (2022) 122961.
[100] Y. Dan, Z. Sheng, L. Zhang, L. Lu, Effects of lifted fuel injection using an upstream ramp of a cavity on scramjet combustion, Aerospace Science and Technology 142 (2023) 108651. https://doi.org/10.1016/j.ast.2023.108651.
[101] T. Roos, A. Pudsey, M. Bricalli, H. Ogawa, Numerical investigation of fuel mixing with upstream crescent cavities in a scramjet combustor, Acta Astronautica 177 (2020) 611–626. https://doi.org/10.1016/j.actaastro.2020.08.022.
[102] T. Roos, A. Pudsey, H. Ogawa, Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor, Acta Astronaut. 187 (2021) 43–60.
[103] C. Wang, Z. Jiang, Z. Hu, J. Lu, Numerical investigation on the flowfield of “swallowtail” cavity for supersonic mixing enhancement, Acta Mech. Sin. 25 (2009) 37–44.
[104] S.H. Kang, Y.J. Lee, S.S. Yang, B. Choi, Effects of flameholder configurations on combustion in scramjet engines, J. Propul. Power 28 (2012) 739–746.
[105] S.H. Kang, Y.J. Lee, S.S. Yang, B. Choi, Scramjet engine combustor tests in a supersonic wind tunnel with a vitiated air heater, in: 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010: p. 7123.
[106] K. Lee, S. Kang, Y. Lee, B. Cha, B. Choi, Effects of fuel injectors and cavity configurations on supersonic combustion, J. Propul. Power 29 (2013) 1052–1063.
[107] T. Handa, A. Nakano, K. Tanigawa, J. Fujita, Supersonic mixing enhanced by cavity-induced three-dimensional oscillatory flow, Exp Fluids 55 (2014) 1711. https://doi.org/10.1007/s00348-014-1711-y.
[108] T. Handa, M. Masuda, M. Kashitani, Y. Yamaguchi, Measurement of number densities in supersonic flows using a method based on laser-induced acetone fluorescence, Exp. Fluids 50 (2011) 1685–1694.
[109] M. Anyoji, F. Akagi, Y. Matsuda, Y. Egami, T. Handa, Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity, Acta Astronautica 188 (2021) 491–504. https://doi.org/10.1016/j.actaastro.2021.08.019.
[110] D. Jian, Z. Qiuru, H. Chao, Numerical investigation of cavity-induced enhanced supersonic mixing with inclined injection strategies, Acta Astronautica 180 (2021) 630–638. https://doi.org/10.1016/j.actaastro.2021.01.012.
[111] L. Zhang, H. Qiao, J. Liang, Y. Wang, M. Ding, L. Yang, M. Sun, Experimental study of scramjet cavity with rear edge slots and its performance in combustion enhancement, Acta Mech. Sin. 40 (2024) 323135. https://doi.org/10.1007/s10409-023-23135-x.