Numerical investigation on geometric sensitivity and flame stabilisation mechanism in H2 fueled two-strut based scramjet combustor

Fuel - Tập 312 - Trang 122847 - 2022
Gautam Choubey1, Parth Gaud1, Abdulnasser Mahmood Fatah2, Yuvarajan Devarajan3
1Department of Mechanical & Aerospace Engineering, Institute of Infrastructure Technology Research and Management (IITRAM) Gujarat 380026, India
2Department of Petroleum Engineering, College of Engineering, Knowledge University, Erbil, Iraq
3Department of Automobile Engineering, Saveetha School of Engineering, SIMATS, Chennai, Tamilnadu 602105, India

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