Abstract
An experimental study on the interaction of weak shock waves with turbulent axisymmetric jets was conducted to explore mixing augmentation during such interactions. The experimental configuration is an axisymmetric nonhomogeneous jet that is processed by weak normal shock waves propagating along the jet axis. Experiments involved three combinations of jet gas and surrounding medium densities spanning density ratios 0.09 ≤ ρ j / ρ ∞ ≤ 1.52. The oncoming shock strengths varied between Mach numbers 1.1 and 1.5. Planar laser-induced Rayleigh light scattering was utilized to obtain jet fluid concentration distributions. These images along with Schlieren photographs indicate that a strong interaction takes place around the jet downstream of the shock wave. In this region, the lateral spread of the jet increases as a result of strong baroclinic vorticity deposited along the jet boundaries. Quantitative analysis of the planar concentration images reveal that the spatial probability distributions of the jet fluid concentration are markedly different for jets with and without shock interaction. Jet fluid concentration levels are lower and more uniform in the regions processed by a shock wave. The degree of mixing enhancement appears to be weakly influenced by shock strength. The reversal of density ratio between jet and surroundings, and the consequent change in the sign of the baroclinic vorticity do not seem to influence the degree of mixing enhancement greatly.
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References
Abd-El-Fattah AM, Henderson LF (1978) Shock waves at a fast-slow gas interface. J. Fluid Mech. 86: 15
Budzinski JM (1992) Planar Rayleigh scattering measurements of shock enhanced mixing. Ph.D. Thesis, California Institute of Technology
Cetegen BM, Hermanson JC (1994) Mixing characteristics of compressible vortex rings interacting with normal shock waves, to appear in the 25th Symp. (Intl.) on Combustion issue of Combust. and Flame
Dosanjh DS, Weeks TM (1965) Interaction of a starting vortex as well as a vortex street with a traveling shock wave. AIAA Journal 3: 216
Haas J-F, Sturtevant B (1987) Interaction of weak shock waves with cylindrical and spherical gas inhomogeneities. J. Fluid Mech. 181: 41–76
Hayakawa K, Smits AJ, Bogdanoff SM (1983) Turbulence measurements in two shock wave/shear layer interactions. In: Dumas R, Fulachier L (eds) IUTAM Symposium on Structure of Complex Turbulent Flows, Springer Verlag
Jacobs JW (1992) Shock-induced mixing of a light gas cylinder. J. Fluid Mech. 234: 629–649
Jahn RG (1956) The refraction of shock waves at a gaseous interface. J. Fluid Mech. 1: 457
Long MB (1993) Multidimensional imaging in combusting flows by Lorenz-Mie, Rayleigh and Raman scattering. In: Taylor AMKP (ed) Instrumentation for Flows with Combustion, Academic Press, San Diego, USA
Marble FE, Hendricks GJ, Zukoski EE (1987) Progress toward shock enhancement of supersonic combustion processes. AIAA Paper 87–1880, AIAA/SAE/ASME/ASEE/ 23rd Joint Propulsion Meeting, San Diego CA
Naumann A, Hermanns E (1973) On the interaction between a shock wave and a vortex field. Noise Mechanisms, AGARD CP–131, 23–1
Ribner HS (1985) Cylindrical sound wave generated by shock-vortex interaction. AIAA J. 23: 1708
Waitz IA, Marble FE, Zukoski EE (1991) Investigation of contoured wall jet injector for hypervelocity. AIAA Paper 91–2265, 28th AIAA/SAE/ASME/ASEE Joint Propulsion Meeting, Sacramento CA
Waitz IA, Marble FE, Zukoski EE (1992) Vorticity generation by contoured wall injectors. AIAA Paper 92–3550, 28th AIAA/SAE/ASME/ASEE Joint Propulsion Meeting, Nashville, TN
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© 1995 Springer-Verlag Berlin Heidelberg
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Alessandri, D.Y., Cetegen, B.M. (1995). Experimental Study of Mixing in a Turbulent Jet/Shock Interaction. In: Brun, R., Dumitrescu, L.Z. (eds) Shock Waves @ Marseille IV. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-79532-9_55
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DOI: https://doi.org/10.1007/978-3-642-79532-9_55
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