Abstract
The supersonic mixing layer flow, consisting of a relatively cold, slow diluted hydrogen stream and a hot, faster air stream, is numerically simulated with detailed transport properties and chemical reaction mechanisms. The evolution of the combustion process in the supersonic reacting mixing layer is observed and unsteady phenomena of ignition, flame propagation and extinction are successfully captured. The ignition usually takes place at the air stream side of braid regions between two vortexes due to much higher temperature of premixed gases. After ignition, the flame propagates towards two vortexes respectively located on the upstream and downstream of the ignition position. The apparent flame speed is 1569.97 m/s, which is much higher than the laminar flame speed, resulting from the effects of expansion, turbulence, vortex stretching and consecutive ignition. After the flame arrives at the former vortex, the flame propagates along the outer region of the vortex in two branches. Then the upper flame branch close to fuel streamside distinguishes gradually due to too fuel-riched premixed mixtures in the front of the flame and the strong cooling effect of the adjacent cool fuel flow, while the lower flame branch continues to propagate in the vortex.
Similar content being viewed by others
References
Cao W, Zhou H. Existence of shocklets in a two-dimensional supersonic mixing layer and its influence on the flow structure. Sci China Ser A-Math, 2001, 44: 1182–1188
Cao W, Zhou H. The enhancement of the mixing of a 2D supersonic mixing layer. Sci China Ser A-Math, 2002, 45: 874–883
Zhao Y X, Yi S H, Tian L F, et al. The fractal measurement of experimental images of supersonic turbulent mixing layer. Sci China Ser G-Phys Mech Astron, 2008, 51: 1134–1143
Yang W B, Zhuang F G, Shen Q, et al. Experimental and numerical study on instability structure of the supersonic mixing layer (Mc=0.5). Sci China Ser G-Phys Mech Astron, 2009, 52: 1624–1631
Yi S H, He L, Zhao Y X, et al. A flow control study of a supersonic mixing layer via NPLS. Sci China Ser G-Phys Mech Astron, 2009, 52: 2001–2006
Zhao Y X, Yi S H, Tian L F, et al. Multiresolution analysis of density fluctuation in supersonic mixing layer. Sci China Tech Sci, 2010, 53: 584–591
Zhao Y X, Yi S H, Tian L F, et al. Density field measurement and approximate reconstruction of supersonic mixing layer. Chin Sci Bull, 2010, 55: 2004–2009
Zhang Y L, Wang B, Zhang H Q. The shock wave refraction in supersonic planar mixing layers.Chin Phys Lett, 2013, 30
Jackson T L, Hussaini M Y. An asymptotic analysis of supersonic reacting mixing layers. Combust Sci Tech, 1988, 57: 129–140
Gosch C E, Jackson T L. Ignition and structure of a laminar diffusion flame in a compressible mixing layer with finite rate chemistry. Phys Fluids A, 1991, 3: 3087–3097
Silva L F F D, Deshaies B, Champion M, et al. Some specific aspects of combustion in supersonic H2-air laminar mixing layers. Combust Sci Tech, 1993, 89: 317–333
Ju Y, Niioka T. Ignition analysis of unpremixed reactants with chain mechanism in a supersonic mixing layer. AIAA J, 1993, 31: 863–868
Ju Y, Niioka T. Reduced kinetic mechanism of ignition for nonpremixed hydrogen/air in a supersonic mixing layer. Combust Flame, 1994, 99: 240–246
Ju Y, Niioka T. Ignition simulation of methane/hydrogen mixtures in a supersonic mixing layer. Combust Flame, 1995, 102: 462–470
Im H G, Lee S R, Law C K. Ignition in the supersonic hydrogen/air mixing layer with reduced reaction mechanisms. AIAA Paper 94-0548, 1994
Im H G, Chao B H, Bechtold J K, et al. Analysis of thermal ignition in a supersonic mixing layer. AIAA J, 1994, 32: 341–349
Nishioka M, Law C K. A numerical study of ignition in the supersonic hydrogen/air laminar mixing layer. Combust Flame, 1997, 108: 199–219
Tien J H, Stalker R J. Release of chemical energy by combustion in a supersonic mixing layer of hydrogen and air. Combust Flame, 2002, 130: 329–348
Han B, Sung C J, Nishioka M. Effect of vitiated air on hydrogen ignition in a supersonic laminar mixing layer. AIAA Paper 02-0332, 2002
Menon S, Fernando E. A numerical study of mixing and chemical heat release in supersonic mixing layers. AIAA Paper 90-0152, 1990
Planche O H, Reynolds W C. Heat release effects on mixing in supersonic reacting free shear-layers. AIAA Paper 92-0092, 1992
Steinberger C J. Model free simulations of a high speed reacting mixing layer. AIAA Paper 92-0257, 1992
Mahle I, Foysi H, Sarkar S, et al. On the turbulence structure in inert and reacting compressible mixing layers. J Fluid Mech, 2007, 593: 171–180
Miao W B, Cheng X L, Wang Q. Analysis of the energy release effects in supersonic reacting flows. Acta Aerodyn Sin, 2008, 26: 339–343
Drummond J P, Rogers R C. A detailed numerical model of a supersonic reacting mixing layer. AIAA Paper 86-1427, 1990
Drummond J P, Mukunda H S. A numerical study of mixing enhancement in supersonic reacting flow fields. AIAA Paper 88-3260, 1990
Drummond J P, Hussaini M Y. Numerical simulation of a supersonic reacting mixing layer. AIAA Paper 87-1325, 1987
Chakraborty D, Mukunda H S, Paul P J. Effect of confinement in high-speed reacting mixing layer. Combust Flame, 2000, 121: 386–389
Chakraborty D, Upadhyaya H V N, Paul P J, et al. A thermo-chemical exploration of a two-dimensional reacting supersonic mixing layer. Phys Fluids, 1997, 9: 3513–3522
Umemura A, Takihana Y. Nonlinear instabilities leading to rapid mixing and combustion in confined supersonic double-shear-layer flow. Symp (Int) Combust, 1998, 27: 2135–2142
Starik A M, Titova N S, Bezgin L V, et al. The promotion of ignition in a supersonic H2-air mixing layer by laser-induced excitation of O2 molecules: Numerical study. Combust Flame, 2009, 156: 1641–1652
Burcat A, Ruscic B. Third Millennium Ideal Gas and Condensed Phase Thermochemical Database for Combustion with Updates from Active Thermochemical Tables. Report No. ANL 05/20 TAE 960, 2005
Poling B E, Prausniz J M, O’Connel J P. The Properties of Gases and Liquids. New York: McGraw-Hill, 2001
Ren Y X, Liu M E, Zhang H X. A characteristic-wise hybrid compact-WENO scheme for solving hyperbolic conservation laws. Comput Phys, 2003, 192: 365–386
Eberhardt S, Imlay S. A diagonal implicit scheme for computing flows with finite-rate chemistry. AIAA Paper 90-1577, 1990
Chi W S, Osher S. Efficient implementation of essentially non-oscillatory shock-capturing schemes. J Comput Phys, 1988, 77: 439–471
Goebel S G, Dutton J C, Krier H, et al. Mean and turbulent velocity measurements of supersonic mixing layers. Exp Fluids, 1990, 8: 263–272
Huson D A, Long L N, Morris P J. Computation of a confined compressible mixing layer. AIAA Paper 95-2173, 1995
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Zhang, Y., Wang, B. & Zhang, H. Ignition, flame propagation and extinction in the supersonic mixing layer flow. Sci. China Technol. Sci. 57, 2256–2264 (2014). https://doi.org/10.1007/s11431-014-5655-5
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s11431-014-5655-5