Hostname: page-component-848d4c4894-x5gtn Total loading time: 0 Render date: 2024-05-03T15:13:12.490Z Has data issue: false hasContentIssue false

Plane blast wave interaction with an elongated straight and inclined heat-generated inhomogeneity

Published online by Cambridge University Press:  19 July 2018

S. Sembian
Affiliation:
Department of Mechanics, KTH - Royal Institute of Technology, SE-100 44, Stockholm, Sweden
M. Liverts
Affiliation:
Department of Mechanics, KTH - Royal Institute of Technology, SE-100 44, Stockholm, Sweden
N. Apazidis*
Affiliation:
Department of Mechanics, KTH - Royal Institute of Technology, SE-100 44, Stockholm, Sweden
*
Email address for correspondence: nap@mech.kth.se

Abstract

The unstable evolution of an elongated elliptically shaped inhomogeneity that is embedded in ambient air and aligned both normal and at an angle to an incident plane blast wave of impact Mach number 2.15 is investigated both experimentally and numerically. The elliptic inhomogeneities and the blast waves are generated using gas heating and exploding wire technique and their interaction is captured optically using shadowgraph method. While two symmetric counter-rotating vortices due to Richtmyer–Meshkov instability are observed for the straight interaction, the formation of a train of vortices similar to Kelvin–Helmholtz instability, introducing asymmetry into the flow field, are observed for an inclined interaction. During the early phase of the interaction process in the straight case, the growth of the counter-rotating vortices (based on the sequence of images obtained from the high-speed camera) and circulation (calculated with the aid of numerical data) are found to be linear in both space and time. Moreover, the normalized circulation is independent of the inhomogeneity density and the ellipse thickness, enabling the formulation of a unique linear fit equation. Conversely, the circulation for an inclined case follows a quadratic function, with each vortex in the train estimated to move with a different velocity directly related to its size at that instant. Two factors influencing the quadratic nature are identified: the reduction in strength of the transmitted shock thereby generating vortices with reduced vorticity, along with the gradual loss of vorticity of the earlier-generated vortices.

Type
JFM Papers
Copyright
© 2018 Cambridge University Press 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Aleksandrov, P. E. 1993 Thermal layer effect in MHD: interaction of a parallel shock with a layer of decreased density. Shock Waves 3 (2), 7378.Google Scholar
Artem’ev, V. I., Bergel’Son, V. I., Medvedyuk, S. A., Orlova, I. V., Nemchinovand, T. I., Rybakov, V. A. & Khazins, V. M. 1993 Vortex flows induced by interaction of a shock wave with thin regions of finite length and reduced density. Fluid Dyn. 28 (3), 411414.Google Scholar
Artem’ev, V. I., Bergel’Son, V. I., Nemchinov, I. V., Orlova, T. I., Smirnov, V. A. & Khazins, V. M. 1989 Change of regime in supersonic flow past an obstacle preceded by a thin channel of reduced density. Fluid Dyn. 24 (5), 779784.Google Scholar
Azarova, O., Knight, D. & Kolesnichenko, Y.2010 Instabilities, vortices and structures characteristics during interaction of microwave filaments with body in supersonic flow. AIAA Paper 1004.Google Scholar
Azarova, O., Knight, D. & Kolesnichenko, Y. 2013 Flow control via instabilities, vortices and steady structures under the action of external microwave energy release. Proc. Inst. Mech. Engrs 227 (9), 14981515.Google Scholar
Bates, K. R., Nikiforakis, N. & Holder, D. 2007 Richtmyer–Meshkov instability induced by the interaction of a shock wave with a rectangular block of SF. Phys. Fluids 19, 036101.Google Scholar
Brouillette, M. 2002 The Richtmyer–Meshkov instability. Annu. Rev. Fluid Mech. 34, 445468.Google Scholar
Ganguly, B. N., Bletzinger, P. & Garscadden, A. 1997 Shock wave damping and dispersion in nonequilibrium low pressure argon plasmas. Phys. Lett. A 230 (3–4), 218222.Google Scholar
Georgievskii, P. Y., Levin, V. A. & Sutyrin, O. G. 2010 Two-dimensional self-similar flows generated by the interaction between a shock and low-density gas regions. Fluid Dyn. 45 (2), 281288.Google Scholar
Georgievskiy, P. Y., Levin, V. A. & Sutyrin, O. G. 2015 Interaction of a shock with elliptical gas bubbles. Shock Waves 25, 357369.Google Scholar
Georgievskii, P. Y., Levin, V. A. & Sutyrin, O. G. 2016 Interaction between a shock wave and a longitudinal low-density gas layer. Fluid Dyn. 51 (5), 696702.Google Scholar
Giordano, J. & Burtschell, Y. 2006 Richtmyer–Meshkov instability induced by shock–bubble interaction: numerical and analytical studies with experimental validation. Phys. Fluids 18, 036102.Google Scholar
Gordeev, V. P., Krasil’Nikov, A. V., Lagutin, V. I. & Otmennikov, V. N. 1996 Experimental study of the possibility of reducing supersonic drag by employing plasma technology. Fluid Dyn. 31 (2), 313317.Google Scholar
Grun, J., Burris, R., Joyce, G., Slinker, S., Huba, J., Evans, K., Manka, C. K., Barthel, J. R. & Wiehe, J. W. 1998 Small-scale laboratory measurement and simulation of a thermal precursor shock. J. Appl. Phys. 83 (5), 24202427.Google Scholar
Haas, J. F. & Sturtevant, B. 1987 Interaction of weak shock waves with cylindrical and spherical inhomogeneities. J. Fluid Mech. 181, 4176.Google Scholar
Jacobs, J. W. 1992 Shock-induced mixing of a light-gas cylinder. J. Fluid Mech. 234, 629649.Google Scholar
Jahn, R. G. 1956 The refraction of shock waves at a gaseous interface. J. Fluid Mech. 1 (5), 457489.Google Scholar
Johnson, R. W. 2016 Handbook of Fluid Dynamics. CRC Press.Google Scholar
Kemm, F. 2015 On two deficiencies of the AUFS scheme for Euler flows and possible fixes. Z. Angew. Math. Mech. J. Appl. Math. Mech. 95, 897910.Google Scholar
Klimov, A. I., Koblov, A. N., Mishin, G. I., Serov, Y. L. & Yavor, I. P. 1982 Shock wave propagation in a glow discharge. Sov. Tech. Phys. Lett. 8 (4), 192194.Google Scholar
Knight, D. 2008 Survey of aerodynamic drag reduction at high speed by energy deposition. J. Propul. Power 24 (6), 11531167.Google Scholar
Knight, D., Azarova, O. & Kolesnichenko, Y. 2009 On details of flow control via characteristics and location of microwave filament during its interaction with supersonic blunt body. In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, pp. 847867.Google Scholar
Kumar, S., Vorobieff, P., Orlicz, G., Palekar, A. & Tomkins, C. 2007 Complex flow morphologies in shock-accelerated gaseous flows. Physica D 235, 2128.Google Scholar
Layes, G., Jourdan, G. & Houas, L. 2003 Distortion of a spherical gaseous interface accelerated by a plane shock wave. Phys. Rev. Lett. 91, 174502.Google Scholar
Layes, G., Jourdan, G. & Houas, L. 2005 Experimental investigation of the shock wave interaction with a spherical gas inhomogeneity. Phys. Fluids 17, 028103.Google Scholar
Layes, G., Jourdan, G. & Houas, L. 2009 Experimental study on a plane shock wave accelerating a gas bubble. Phys. Fluids 21, 074102.Google Scholar
Layes, G. & LeMetayer, O. 2007 Quantitative numerical and experimental studies of the shock accelerated heterogeneous bubbles motion. Phys. Fluids 19, 042105.Google Scholar
MacCormack, R. W. 2011 The carbuncle cfd problem. In Proceedings of the 49th AIAA Aerospace Sciences Meeting, pp. 381392.Google Scholar
Macheret, S. O., Ionikh, Y. Z., Chernysheva, N. V., Yalin, A. P., Martinelli, L. & Miles, R. B. 2001 Shock wave propagation and dispersion in glow discharge plasmas. Phys. Fluids 13 (9), 26932705.Google Scholar
Markstein, G. H. 1957 Flow disturbances induced near a slightly wavy contact surface, or flame front, traversed by a shock wave. J. Aerosp. Sci. 24, 238239.Google Scholar
Meshkov, E. E. 1969 Instability of the interface of two gases accelerated by a shock wave. Fluid Dyn. 4, 101104.Google Scholar
Mirels, H.1986 Interaction of moving shock with thin stationary thermal layer. Tech. Rep., Aerospace Corp El Segundo Ca Aerophysics Lab.Google Scholar
Nemchinov, I. V., Artem’ev, V. I., Bergel’Son, V. I., Khazins, V. M., Orlova, T. I. & Rybakov, V. A. 1994 Rearrangement of the bow shock shape using a hot spike. Shock Waves 4 (1), 3540.Google Scholar
Niederhaus, J. H., Greenough, J. A, Oakley, J. G., Ranjan, D., Anderson, M. H. & Bonazza, R. 2007 A computational parameter study for the three-dimensional shock–bubble interaction. Phys. Rev. Lett. 98, 024502.Google Scholar
Picone, J. M. & Boris, J. P. 1988 Vorticity generation by shock propagation through bubbles in a gas. J. Fluid Mech. 189, 2351.Google Scholar
Picone, J. M., Oran, E. S., Boris, J. P. & Young, T. R. Jr. 1984 Theory of vorticity generation by shock wave and flame interactions. Tech. Rep., Naval Research Lab Washington DC.Google Scholar
Quirk, J. J. & Karni, S. 1996 On the dynamics of a shock–bubble interaction. J. Fluid Mech. 318, 129163.Google Scholar
Ranjan, D., Anderson, M., Oakley, J. & Bonazza, R. 2005 Experimental investigation of a strongly shocked gas bubble. Phy. Rev. Lett. 94, 184507.Google Scholar
Ranjan, D., Niederhaus, J., Motl, B., Anderson, M., Oakley, J. & Bonazza, R. 2007 Experimental investigation of primary and secondary features in high-Mach number shock–bubble interaction. Phy. Rev. Lett. 98, 024502.Google Scholar
Ranjan, D., Oakley, J. & Bonazza, R. 2011 Shock–bubble interactions. Annu. Rev. Fluid Mech. 43, 117140.Google Scholar
Ray, J., Samtaney, R. & Zabusky, N. J. 2000 Shock interactions with heavy gaseous elliptic cylinders: two leeward-side shock competition modes and a heuristic model for interfacial circulation deposition at early times. Phys. Fluids 12, 707716.Google Scholar
Richtmyer, R. D. 1960 Taylor instability in shock acceleration of compressible fluids. Commun. Pure Appl. Maths 13, 297319.Google Scholar
Rudinger, G. & Somers, L. M. 1960 Behaviour of small regions of different gases carried in accelerated gas flows. J. Fluid Mech. 7, 161176.Google Scholar
Samtaney, R. & Zabusky, N. J. 1994 Circulation deposition on shock-accelerated planar and curved density-stratified interfaces: models and scaling laws. J. Fluid Mech. 269, 4578.Google Scholar
Sembian, S., Liverts, M. & Apazidis, N. 2018 Plane blast wave propagation in air with a transverse thermal inhomogeneity. Eur. J. Mech. (B/Fluids) 67, 220230.Google Scholar
Stephan, K. & Laesecke, A. 1985 The thermal conductivity of fluid air. J. Phys. Chem. Ref. Data 14, 227234.Google Scholar
Sun, M. & Takayama, K. 2003 An artificially upstream flux vector splitting scheme for the Euler equations. J. Comput. Phys. 189, 305329.Google Scholar
Svetsov, V. 2001 Vortical regime of the flow behind the bow shock wave. Shock Waves 11 (3), 229244.Google Scholar
Tchuen, G., Fogang, F., Burtschell, Y. & Woafo, P. 2014 A hybrid numerical method and its application to inviscid compressible flow problems. Comput. Phys. Commun. 185, 479488.Google Scholar
Tomkins, C., Prestridge, K., Rightley, P., Marr-Lyon, M., Vorobieff, P. & Benjamin, R. 2003 A quantitative study of the interaction of two Richtmyer–Meshkov-unstable gas cylinders. Phys. Fluids 15, 9861004.Google Scholar
Tretyakov, P., Tupikin, A. & Zudov, V. 2012 Interaction of a shock wave with a contact discontinuity for local heat release in a flow. In 28th International Symposium on Shock Waves, pp. 887892. Springer.Google Scholar
Wang, T., Bai, J., Li, P. & Liu, K. 2010 Large-eddy simulations of the Richtmyer–Meshkov instability of rectangular interfaces accelerated by shock waves. Sci. Chin. Phys. Mech. Astron. 53, 905914.Google Scholar
Yang, J., Kubota, T. & Zukoski, E. E. 1993 Applications of shock-induced mixing to supersonic combustion. AIAA J. 31, 854862.Google Scholar
Yang, J., Kubota, T. & Zukoski, E. E. 1994 A model for characterization of a vortex pair formed by shock passage over a light-gas inhomogeneity. J. Fluid Mech. 258, 217244.Google Scholar
Zabusky, N. J. 1999 Vortex paradigm for accelerated inhomogeneous flows: visiometrics for the Rayleigh–Taylor and Richtmyer–Meshkov environments. Annu. Rev. Fluid Mech. 31, 495536.Google Scholar
Zhai, Z., Wang, M., Si, T. & Luo, X. 2014 On the interaction of a planar shock with a light polygonal interface. J. Fluid Mech. 757, 800816.Google Scholar
Zou, L., Liu, C., Tan, D., Huang, W. & Luo, X. 2010 On interaction of shock wave with elliptic gas cylinder. J. Vis. 13, 347353.Google Scholar
Zudov, V. N. 2010 Interaction of shock wave with subsonic heated layer. Tech. Phys. Lett. 36 (9), 868871.Google Scholar
Zudov, V. N., Tret’yakov, P. K., Tupikin, A. V. & Yakovlev, V. I. 2003 Supersonic flow past a thermal source. Fluid Dyn. 38 (5), 782793.Google Scholar