[1]JIANG Z L.Standing oblique detonation for hypersonic propulsion: A review[J].Progress in Aerospace Sciences, 2023, 143(143):100955-100955
[2]YANG P F, NG H D, TENG H H, et al.Initiation structure of oblique detonation waves behind conical shocks[J].Physics of Fluids, 2017, 29(8):1-10
[3]杨鹏飞,张子健,杨瑞鑫,等.斜爆轰发动机的推力性能理论分析[J].力学学报, 2021, 53(10):2853-2864
[4]YANG P F, ZHANG Z J, YANG R X, et al.Theoretical analysis of thrust performance in oblique detonation engines[J].Acta Mechanica Sinica, 2021, 53(10):2853-2864
[5]HE G S, FENG Z L, WANG K L, et al.Unsteady wave characteristics of oblique detonation wave in a contraction–expansion channel[J].International Journal of Hydrogen Energy, 2024, 71:999-1005
[6]滕宏辉,姜宗林.斜爆轰的多波结构及其稳定性研究进展[J].力学进展, 2020, 50(0):50-92
[7]TENG H H, JIANG Z L.Multi-wave configurations and stability of oblique detonation: Research advances , : 50–92. (in Chinese)[J].Advances in Mechanics, 2020, 50(0):50-92
[8]YANG P F, YU D H, CHEN Z, et al.Effects of thermal stratification on detonation development in hypersonic reactive flows[J].PHYSICAL REVIEW FLUIDS, 2024, 9(8):083202-083202
[9]张博, 白春华.气相爆轰动力学特征研究进展[J].中国科学物理学·力学·天文学, 2014, 44(7):665-681
[10]ZHANG B, BAI C H.Advances in gaseous detonation dynamics[J].Science China Physics, Mechanics & Astronomy, 2014, 44(7):665-681
[11]YANG P F, NG H D, TENG H H.Numerical study of wedge-induced oblique detonations in unsteady flow[J].Journal of fluid mechanics, 2019, 876(1):264-287
[12]TENG H H, LIU S Y, LI Z Z, et al.Effect of ozone addition on oblique detonations in hydrogen-air mixtures[J].Applied Thermal Engineering, 2024, 240(0):122292-122292
[13]YANG P F, TENG H H, NG H D et al.A numerical study on the instability of oblique detonation waves with a two-step induction–reaction kinetic model[J].Proceedings of the Combustion Institute, 2019, 37(3):3537-3544
[14]SUN J, YANG P F, TIAN B L, et al.Evolution and Control of Oblique Detonation Wave Structure in Unsteady Inflow[J].AIAA JOURNAL, 2023, 61(11):4808-4820
[15]YANG P F, TENG H H, JIANG Z L, et al.Effects of inflow Mach number on oblique detonation initiation with a two step induction_reaction kinetic model[J].Combustion & Flame, 2018, 193(0):246-256
[16]TENG H H, NG H D, JIANG Z L.Initiation characteristics of wedge-induced oblique detonation waves in a stoichiometric hydrogen-air mixture[J].Proceedings of the Combustion Institute, 2017, 36(2):2735-2742
[17]PRATT D T, HUMPHREY J W et al.Morphology of standing oblique detonation waves[J].Propul. Power, 1991, 7(5):837-845
[18]TENG H H, ZHANG Y H, YANG P F, JIANG Z L.Oblique detonation wave triggered by a double wedge in hypersonic flow[J].Chinese Journal of Aeronautics, 2022, 35(4):176-184
[19]FANG Y, ZHANG Z, HU Z, DENG X.Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures[J].Aerosp.Sci.Technol, 2019, 92(0):676-684
[20]YANG L, YUE L J, ZHANG Q F.Onset of Oblique Detonation Waves for a Cavity-Based Wedge[J].AIAA Journal, 2022, 60(5):2836-2849
[21]QIN Q Y, ZHANG X B.A novel method for trigger location control of the oblique detonation wave by a modified wedge[J].Combustion & Flame, 2018, 197(0):65-77
[22]ZHANG Y C, XIANG G X.Investigations on the initiation characteristics of radical-assisted oblique detonation waves generated by plasma discharges[J].Aerospace Science and Technology, 2024, 153:109466-109466
[23]LI H, LI J, XIONG C, et al.Investigation of hot jet on active control of oblique detonation waves[J].Chin. J. Aeronaut, 2020, 33(3):861-869
[24]QIN Q, ZHANG X.Study on the initiation characteristics of the oblique detonation wave by a co-flow hot jet[J].Acta Astronaut, 2020, 177(0):86-95
[25]WANG A, BIAN J, TENG H H.Numerical study on initiation of oblique detonation wave by hot jet[J].Applied Thermal Engineering, 2022, 213(Suppl C):118679-118679
[26]ZHANG W, ZHANG Z J, JIANG Z L, et al.Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition[J].AIP Advances, 2021, 11(12):125119-125119
[27]XIN Y, SHANG J, XIANG G, et al.Investigation on Accelerated Initiation of Oblique Detonation Wave Induced by Laser-Heating Hot-Spot[J].Aerospace, 2024, 11(6):485-485
[28]WILSON G J, MACCORMACK R W.Modeling supersonic combustion using a fully implicit numerical method[J].AIAA Journal, 1992, 30(4):1008-1015
[29]JACHIMOWSKI C J.Analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion[J]., 1988, :-
[30]郗雪辰, 牛淑贞, 杨鹏飞, 等.氢气燃料斜爆轰发动机内波系对楔面调控的动态响应特性[J].航空学报, 2024, 45(22):126-140
[31]XI X C, NIU S Z, YANG P F, et al.Dynamic response characteristics of wave system to wedge angle modulation in hydrogen-fueled oblique detonation engines[J].Acta Aeronautica et Astronautica Sinica, 2024, 45(22):126-140
[32]TAYLOR G, The Formation of a Blast Wave by a Very Intense Explosion.ITheoretical Discussion [I]. Proceedings of the Royal Society of LondonSeries A, Mathematical and Physical Sciences, 1950, 201(1065): 159-174.
[33]KIELKOPF J F.Spectroscopic study of laser-produced plasmas in hydrogen[J].Physical Review E, 1995, 52(2):2013-2024
[34]FANG Y, ZHANG Z, HU Z.Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures[J].International Journal of Hydrogen Energy, 2019, 44(41):23429-23435
[35]MIAO S K, XU D, SONG T L, et al.Shock wave Boundary Layer Interactions in Wedge-induced Oblique Detonations[J].Combustion Science and Technology, 2020, 192(12):2345-2370
[36]sLIU Y, CHEN W Q, WANG L, et al.Oblique Detonation Initiation by an Instantaneous Energy Source in High-Speed Wedge Flows[J].AIAA JOURNAL, 2021, 59(11):4794-4799