Numerical investigation on geometric sensitivity and flame stabilisation mechanism in H2 fueled two-strut based scramjet combustor
Tài liệu tham khảo
Billig, 1993, Research on supersonic combustion, J Propuls Power, 9, 499, 10.2514/3.23652
Curran, 2001, Scramjet engines: the first forty years, J. Propuls. Power, 17, 1138, 10.2514/2.5875
Cecere, 2011, Hydrogen/air supersonic combustion for future hypersonic vehicles, Int J Hydrogen Energy, 36, 11969, 10.1016/j.ijhydene.2011.06.051
Choubey, 2017, Numerical studies on the performance of scramjet combustor with alternating wedge-shaped strut injector, Int J Turbo Jet Eng, 34, 11
Lee, 2006, of dual transverse injection in scramjet combustor, Part 1: mixing, J Propuls Power, 22, 1012, 10.2514/1.14180
Gerdroodbary, 2020, 1
Watanabe, 2011, Numerical study on turbulent structure of transverse jet into a supersonic flow
Oevermann, 2000, Numerical investigation of turbulent hydrogen combustion in a scramjet using flamelet modelling, Aero Sci Technol, 4, 463, 10.1016/S1270-9638(00)01070-1
Génin, 2010, Simulation of turbulent mixing behind a strut injector in supersonic flow, AIAA J, 48, 526, 10.2514/1.43647
Huang, 2015, Wei X-g. Large eddy simulation of strut enhanced mixing for supersonic combustion, J Solid Rocket Technol, 38, 664
Huang, 2015, Wei X-g. Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor, Int J Hydrogen Energy, 40, 9815, 10.1016/j.ijhydene.2015.06.011
Pandey, 2015, Computational analysis of hypersonic combustor using strut injector at flight Mach 7, Combust Sci Technol, 187, 1392, 10.1080/00102202.2015.1035371
Pandey, 2016, Numerical investigation on hydrogen-fueled scramjet combustor with parallel strut fuel injector at a flight Mach number of 6, J Appl Fluid Mech, 9, 1215, 10.18869/acadpub.jafm.68.228.24082
Choubey, 2016, Effect of variation of angle of attack on the performance of two-strut scramjet combustor, Int J Hydrogen Energy, 41, 11455, 10.1016/j.ijhydene.2016.04.048
Choubey, 2017, Effect of parametric variation of strut layout and position on the performance of a typical two-strut based scramjet combustor, Int J Hydrogen Energy, 42, 10485, 10.1016/j.ijhydene.2017.03.014
Choubey, 2016, Investigation on the effects of operating variables on the performance of two-strut scramjet combustor, Int J Hydrogen Energy, 41, 20753, 10.1016/j.ijhydene.2016.09.157
Choubey, 2017, Effect of different strut + wall injection techniques on the performance of two-strut scramjet combustor, Int J Hydrogen Energy, 42, 13259, 10.1016/j.ijhydene.2017.04.024
Choubey, 2016, Computational simulation of multi-strut central lobed injection of hydrogen in a scramjet combustor, Perspect Sci, 8, 222, 10.1016/j.pisc.2016.04.032
Choubey, 2017, Computational investigation of multi-strut injection of hydrogen in a scramjet combustor, Mater Today Proc., 4, 2608, 10.1016/j.matpr.2017.02.115
Li, 2019, Numerical investigation on the performance of scramjet combustor with a novel strut configuration, Appl Therm Eng, 159, 113894, 10.1016/j.applthermaleng.2019.113894
Ben-Yakar, 2001, Cavity flame-holders for ignition and flame stabilization in scramjets: an overview, J Propul Power, 17, 869, 10.2514/2.5818
Gruber, 2001, Fundamental studies of cavity based flameholder concepts for supersonic combustors, J Propuls Power, 17, 146, 10.2514/2.5720
Choubey, 2019, Recent advances in cavity-based scramjet engine a brief review, Int J Hydrogen Energy, 44, 13895, 10.1016/j.ijhydene.2019.04.003
Wang, 2013, Experimental study of oscillations in a scramjet combustor with cavity flameholders, Exp Therm Fluid Sci, 45, 259, 10.1016/j.expthermflusci.2012.10.013
Sun, 2008, Flame characteristics in supersonic combustor with hydrogen injection upstream of cavity flameholder, J Propul Power, 24, 688, 10.2514/1.34970
Wang, 2013, Large-Eddy/Reynolds-averaged Navier-Stokes simulation of combustion oscillations in a cavity-based supersonic combustor, Int J Hydrogen Energy, 38, 5918, 10.1016/j.ijhydene.2013.02.100
Mahto, 2016, Effect of variation of length-to-depth ratio and Mach number on the performance of a typical double cavity scramjet combustor, Acta Astronaut, 128, 540, 10.1016/j.actaastro.2016.08.010
Wang, 2013, Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor, Int J Hydrogen Energy, 38, 12078, 10.1016/j.ijhydene.2013.06.132
Billig FS, Orth RC, Schetz JA. The Interaction and Penetration of Gaseous Jets in Supersonic Flow. NASA CR-1386, July 1969.
Schetz, 1991, Analysis of slot injection in hypersonic flow, J Propuls Power, 7, 115, 10.2514/3.23301
Huang, 2013, Progress in research on mixing techniques for transverse injection flow fields in supersonic crossflows, J Zhejiang Univ Sci A, 14, 554, 10.1631/jzus.A1300096
Huang, 2016, Transverse jet in supersonic crossflows, Aero Sci Technol, 50, 183, 10.1016/j.ast.2016.01.001
Dong, 2019, Influence of the secondary flow control on the transverse gaseous injection flow field properties in a supersonic flow, Acta Astronaut, 165, 150, 10.1016/j.actaastro.2019.08.028
Huang, 2021, Design exploration on the mixing augmentation induced by the oblique shock wave and a novel step in a supersonic flow, Acta Astronaut, 180, 622, 10.1016/j.actaastro.2020.12.058
Huang, 2013, Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows, Acta Astronaut., 84, 141, 10.1016/j.actaastro.2012.11.011
Du, 2021, Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine, Aero Sci Technol, 108, 106413, 10.1016/j.ast.2020.106413
Athithan, 2021, The combustion characteristics of double ramps in a strut-based scramjet combustor, Energies, 14, 831, 10.3390/en14040831
Sun, 2021, Mixing efficiency of hydrogen multijet through backward-facing steps at supersonic flow, Int J Hydrogen Energy, 46, 16075, 10.1016/j.ijhydene.2021.02.030
Barzegar Gerdroodbary, 2016, The influence of micro air jets on mixing augmentation of transverse hydrogen jet in supersonic flow, Int J Hydrogen Energy, 41, 22497, 10.1016/j.ijhydene.2016.08.185
Barzegar Gerdroodbary, 2017, Characteristics of transverse hydrogen jet in presence of multi air jets within scramjet combustor, Acta Astronaut, 132, 25, 10.1016/j.actaastro.2016.11.041
Gerdroodbary MB, Amini Y, Ganji DD, Takam MR. The flow feature of transverse hydrogen jet in presence of micro air jets in supersonic flow. Adv Space Res 2017; 59:1330-40.
Gerdroodbary, 2021, Computational investigation of multi hydrogen jets at inclined supersonic flow, Int J Energy Res, 45, 1661, 10.1002/er.5821
Barzegar Gerdroodbary, 2016, Comparison of the single/multi transverse jets under the influence of shock wave in supersonic crossflow, Acta Astronaut, 123, 283, 10.1016/j.actaastro.2016.03.031
Chang, 2018, Research progress on strut-equipped supersonic combustors for scramjet application, Prog Aerosp Sci, 103, 1, 10.1016/j.paerosci.2018.10.002
Qiu, 2020, Flowing residence characteristics in a dual-mode scramjet combustor equipped with strut flame holder, Aero Sci Technol, 99, 105718, 10.1016/j.ast.2020.105718
Zhang, 2019, Flame propagation and flashback characteristics in a kerosene fueled supersonic combustor equipped with strut/wall combined fuel injectors, Aero Sci Technol, 93, 105303, 10.1016/j.ast.2019.105303
Waidmann, 1995, Supersonic combustion of hydrogen/air in a scramjet combustion chamber, Space Technol, 15, 421, 10.1016/0892-9270(95)00017-8
Waidmann, 1994, 629
Ingenito, 2010, Physics and regimes of supersonic combustion, AIAA J, 48, 515, 10.2514/1.43652
Sujith, 2013, Effect of trailing ramp angles in strut-based injection in supersonic flow, J Propuls Power, 29, 66, 10.2514/1.B34532
Masuya, 1995, Ignition and combustion performance of scramjet combustors with fuel injection struts, J Propuls Power, 11, 301, 10.2514/3.51425
Dharavath, 2013, Thermochemical exploration of hydrogen combustion in generic scramjet combustor, Aero Sci Technol., 24, 264, 10.1016/j.ast.2011.11.014
Gerlinger, 2000, Numerical investigation of hydrogen strut injections into supersonic airflows, J Propuls Power, 16, 22, 10.2514/2.5559
Dinde, 2006, 3D numerical simulation of the supersonic combustion of H2, Aeronaut J, 110, 773, 10.1017/S0001924000001640
Luo SB, Huang W, Qin H, Wang ZG, Liu J, Xia ZX, Lei J, Pourkashanian M, Ma L, Ingham DB, Luo WL. Investigation of turbulent models for the flow field from a typical strut-based scramjet combustor. Proceedings of ASME Turbo Expo 2011, Vancouver, Canada (2011).
Huang, 2015, Investigation on the effect of strut configurations and locations on the combustion performance of a typical scramjet combustor, J Mech Sci Technol, 29, 5485, 10.1007/s12206-015-1150-6
Huang, 2011, Liu Jun. Parametric effects on the combustion flow field of a typical strut-based scramjet combustor, Chin Sci Bull, 56, 3871, 10.1007/s11434-011-4823-2
ANSYS, Inc. (2016) ANSYS Fluent User’s Guide, Release 17.2.
Bao, 2012, Effects of strut swept angle on the drag of scramjet, Proc Inst Mech Eng, G J Aerosp Eng, 226, 455, 10.1177/0954410011409658
Zong, 2015, Effect of fuel injection allocation on the combustion characteristics of a cavity-strut model scramjet, J Aerosp Eng, 28, 04014050, 10.1061/(ASCE)AS.1943-5525.0000374
Bao, 2014, Effects of upstream strut on the combustion of liquid kerosene in a model cavity scramjet, Proc Inst Mech Eng, G J Aerosp Eng, 228, 2323, 10.1177/0954410013515370
Feng, 2017, Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor, Aerosp Sci Technol, 64, 213, 10.1016/j.ast.2017.02.002
Feng, 2017, Numerical studies for performance improvement of a variable geometry dual mode combustor by optimizing deflection angle, Aerosp Sci Technol, 68, 320, 10.1016/j.ast.2017.05.025
Zhang, 2017, Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor, Acta Astronaut, 137, 44, 10.1016/j.actaastro.2017.03.023
Micka, 2009, Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder, Proc Combust Inst, 32, 2397, 10.1016/j.proci.2008.06.192
Sun, 2020
Sun M B, Wang H, Wang Z, Geng H, Liang J, Liu W, Bai X. Experimental and numerical study on flame stabilization in a supersonic combustor with hydrogen injection upstream of cavity flameholders. In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2009 AIAA-2009-5187.
Wang, 2016, Large Eddy Simulation of the flame stabilization process in a scramjet combustor with rearwall-expansion cavity, Int J Hydrogen Energy, 41, 19278, 10.1016/j.ijhydene.2016.09.012
Yang, 2015, Numerical and experimental study on flame structure characteristics in a supersonic combustor with dual-cavity, Acta Astronaut, 117, 376, 10.1016/j.actaastro.2015.09.005
Yang, 2016, Numerical simulation on ignition transients of hydrogen flame in a supersonic combustor with dual-cavity, Int J Hydrogen Energy, 41, 690, 10.1016/j.ijhydene.2015.11.115
Wang, 2014, Experimental and numerical investigation of cavity-based supersonic flow and combustion, Proc IMechE Part G: J Aerospace Eng, 228, 781
Wang, 2014, Review of cavity-stabilized combustion for scramjet applications, Proc Inst Mech Eng, Part G: J Aerospace Eng, 228, 2718, 10.1177/0954410014521172
Wang, 2014, Numerical study on supersonic mixing and combustion with hydrogen injection upstream of a cavity flameholder, Heat Mass Transfer, 50, 211, 10.1007/s00231-013-1227-7
Wang, 2014, Simulations of combustion with normal and angled hydrogen injection in a cavity-based supersonic combustor, Proc I MechE Part G: J Aerospace Eng, 228, 530, 10.1177/0954410013475567
Choubey, 2017, A brief review on the recent advances in scramjet engine, AIP Conf Proc, 1859, 10.1063/1.4990189
Choubey, 2018, Effect of variation of inlet boundary conditions on the combustion flow-field of a typical double cavity scramjet combustor, Int J Hydrogen Energy, 43, 8139, 10.1016/j.ijhydene.2018.03.062
Pandey, 2017, Effect of variation of hydrogen injection pressure and inlet air temperature on the flow-field of a typical double cavity scramjet combustor, Int J Hydrogen Energy, 42, 20824, 10.1016/j.ijhydene.2017.07.026
Choubey, 2018, Composite materials used in Scramjet-a review, Mater Today Proc, 5, 1321, 10.1016/j.matpr.2017.11.217
Choubey, 2018, Effect of different wall injection schemes on the flow-field of hydrogen fuelled strut-based scramjet combustor, Acta Astronaut, 145, 93, 10.1016/j.actaastro.2018.01.034
Choubey, 2020, Recent research progress on transverse injection technique for scramjet applications-a brief review, Int J Hydrogen Energy., 45, 27806, 10.1016/j.ijhydene.2020.07.098
Li, 2020, Influence of backward-facing step on the mixing efficiency of multi microjets at supersonic flow, Acta Astronaut, 175, 37, 10.1016/j.actaastro.2020.05.003
Liu, 2020, Computational study of the multi hydrogen jets in presence of the upstream step in a Ma= 4 supersonic flow, Int J Hydrogen Energy., 45, 31118, 10.1016/j.ijhydene.2020.08.017
Choubey, 2021, Numerical investigation on mixing improvement mechanism of transverse injection based scramjet combustor, Acta Astronaut., 188, 426, 10.1016/j.actaastro.2021.08.008
Liu, 2020, Effect of strut angle on performance of hydrogen multi-jets inside the cavity at combustion chamber, Int J Hydrogen Energy, 45, 31179, 10.1016/j.ijhydene.2020.08.124
Jiang, 2020, Effect of free stream angle on mixing performance of hydrogen multi-jets in supersonic combustion chamber, Int J Hydrogen Energy., 45, 25426, 10.1016/j.ijhydene.2020.06.055
Jiang, 2021, Influence of trapezoidal lobe strut on fuel mixing and combustion in supersonic combustion chamber, Aerosp Sci Technol, 116, 106841, 10.1016/j.ast.2021.106841
Jiang, 2020, Effect of cavity back height on mixing efficiency of hydrogen multi-jets at supersonic combustion chamber, Int J Hydrogen Energy., 45, 27828, 10.1016/j.ijhydene.2020.07.001
Wu, 2017, Numerical investigation on flame stabilization in DLR hydrogen supersonic combustor with strut injection, Combust Sci Technol, 189, 2154, 10.1080/00102202.2017.1365847
Wu, 2019, Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor, Proc Combust Inst, 37, 3685, 10.1016/j.proci.2018.07.097
Wu K, Zhang P, Yao W, Fan X. LES study of flame stabilization in DLR hydrogen supersonic combustor with strut injection. In 21st AIAA International Space Planes and Hypersonics Technologies Conference 2017 AIAA 2017-2322.
Yao, 2018, Modeling analysis of an actively cooled scramjet combustor under different kerosene/air ratios, J Propul Power, 34, 975, 10.2514/1.B36866
Yao W, Wu K, Lee Y, Fan X. Influence of chemical mechanisms on supersonic combustion characteristics fueled by kerosene. In 2018 Joint Propulsion Conference 2018 AIAA 2018-4740.
Yao, 2019, Influences of domain symmetry on supersonic combustion modelling, J Propul Power, 35, 451, 10.2514/1.B37227
Fan E, Wu K, Lee Y, Yao W, Fan X. Full-scale Improved Delayed Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion. In 2018 Joint Propulsion Conference 2018 AIAA 2018-4542.
Yuan, 2015, Study on flame stabilization in a dual-mode combustor using optical measurements, J Propul Power, 31, 1524, 10.2514/1.B35689
Menter, 1994, Two-equation eddy-viscosity turbulence models for engineering applications, AIAA J, 32, 1598, 10.2514/3.12149
Gerlinger, 2008, Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity, Aero Sci Technol, 12, 159, 10.1016/j.ast.2007.04.003
Nithish Reddy, 2015, Numerical investigations on development of scramjet combustor, J Aerosp Eng, 28, 10.1061/(ASCE)AS.1943-5525.0000456
Qin, 2019, A novel method for flame stabilization in a strut-based scramjet combustor, Combust Flame, 210, 292, 10.1016/j.combustflame.2019.08.038