Spark-enhanced ignition and flame stabilization in an ethylene-fueled scramjet combustor with a rear-wall-expansion geometry
Tóm tắt
Từ khóa
Tài liệu tham khảo
Ben-Yakar, 2001, Cavity flame-holders for ignition and flame stabilization in Scramjets: an overview, J. Propls. Power, 17, 869, 10.2514/2.5818
Mathur, 2001, Supersonic combustion experiments with a cavity-based fuel injector, J. Propls. Power, 17, 1305, 10.2514/2.5879
Etheridge, 2017, Effect of flow distortion on fuel/air mixing and combustion in an upstream-fueled cavity flameholder for a supersonic combustor, Exp. Therm Fluid Sci., 88, 461, 10.1016/j.expthermflusci.2017.06.013
Wang, 2013, Experimental study of oscillations in a scramjet combustor with cavity flameholder, Exp. Therm Fluid Sci., 45, 259, 10.1016/j.expthermflusci.2012.10.013
Ukai, 2014, Effectiveness of jet location on mixing characteristics inside a cavity in supersonic flow, Exp. Therm Fluid Sci., 52, 59, 10.1016/j.expthermflusci.2013.08.022
Wang, 2014, Review of cavity-stabilized combustion for scramjet applications, J. Aerospace Eng., Proceed. Institut. Mech. Eng. Part G, 228, 2718, 10.1177/0954410014521172
Barnes, 2015, Cavity-based flameholding for chemically-reacting supersonic flow, Prog. Aerosp. Sci., 76, 24, 10.1016/j.paerosci.2015.04.002
Sun, 2012, Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition, Exp. Therm Fluid Sci., 43, 90, 10.1016/j.expthermflusci.2012.03.028
Allison, 2017, Investigation of supersonic combustion dynamics via 50 kHz CH chemiluminescence imaging, Proc. Combust. Inst., 36, 10.1016/j.proci.2016.08.039
Miller, 2017, Investigation of transient ignition processes in a model scramjet pilot cavity using simultaneous 100 kHz formaldehyde planar laser-induced fluorescence and CH* chemiluminescence imaging, Proc. Combust. Inst., 36, 2865, 10.1016/j.proci.2016.07.060
Yuan, 2017, Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH chemiluminescence, Proc. Combust. Inst., 36, 2919, 10.1016/j.proci.2016.07.040
Savelkin, 2015, Ignition and flameholding in a supersonic combustor by an electrical discharge combined with a fuel injector, Combust. Flame, 162, 825, 10.1016/j.combustflame.2014.08.012
Kim, 2017, Combustion characteristics of small-scaled duct combustor in low enthalpy supersonic flow, Proc. Combust. Inst., 36, 2873, 10.1016/j.proci.2016.06.083
R.T. Milligan, J. Liu, C.J. Tam, 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, Nashville, Tennessee, 2012.
R.T. Milligan, D.R. Eklund, j.M. Wolff, M. Gruber, T. Mathur, Dual mode scramjet combustor: analysis of two configurations, in: 48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Oriando, Florida, 2010.
Milligan, 2011, Dual-mode scramjet combustor: numerical analysis of two flowpaths, J. Propul. Power, 27, 10.2514/1.B34178
Cai, 2016, Experimental investigation on ignition schemes of a supersonic combustor with the rearwall-expansion cavity, Acta Astronaut., 123, 181, 10.1016/j.actaastro.2016.03.008
Cai, 2014, Investigation of the spark ignition enhancement in a supersonic flow, Mod. Phys. Lett. B, 28, 1, 10.1142/S0217984914502261
Cai, 2017, Experiments on flame stabilization in a Scramjet Combustor with a rear-wall-expansion cavity, Int. J. Hydrogen Energy, 42, 26752, 10.1016/j.ijhydene.2017.09.059
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
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
Cai, 2016, Large Eddy Simulation of the fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity, Acta Astronaut., 126, 375, 10.1016/j.actaastro.2016.05.010
Li, 2014, Ignition transients in a scramjet engine with air throttling part 1: nonreacting flow, J. Propul. Power, 30, 438, 10.2514/1.B34763
Li, 2015, Ignition transients in a Scramjet engine with air throttling Part II: reacting flow, J. Propul. Power, 31, 79, 10.2514/1.B35269