Hostname: page-component-586b7cd67f-dlnhk Total loading time: 0 Render date: 2024-11-20T09:22:21.840Z Has data issue: false hasContentIssue false

Circulation deposition on shock-accelerated planar and curved density-stratified interfaces: models and scaling laws

Published online by Cambridge University Press:  26 April 2006

Ravi Samtaney
Affiliation:
Department of Mechanical and Aerospace Engineering, and CAIP Center, Rutgers University, Piscataway, NJ 08855, USA
Norman J. Zabusky
Affiliation:
Department of Mechanical and Aerospace Engineering, and CAIP Center, Rutgers University, Piscataway, NJ 08855, USA

Abstract

Vorticity is deposited baroclinically by shock waves on density inhomogeneities. In two dimenslons, the circulation deposited on a planar interface may be derived analytically using shock polar analysis provided the shock refraction is regular. We present analytical expressions for Γ′, the circulation deposited per unit length of the unshocked planar interface, within and beyond the regular refraction regime. To lowest order, Γ′ scales as \[ \Gamma^\prime\propto (1-\eta^{-\frac{1}{2}})(\sin\alpha)(1+M^{-1}+2M^{-2})(M-1)(\gamma^{\frac{1}{2}}/\gamma + 1)\] where M is the Mach number of the incident shock, η is the density ratio of the gases across the interface, α is the angle between the shock and the interface and γ is the ratio of specific heats for both gases. For α ≤ 30°, the error in this approximation is less than 10% for 1.0 < M ≤ 1.32 for all η > 1, and 5.8 ≤ η ≤ 32.6 for all M. We validate our results by quantification of direct numerical simulations of the compressible Euler equations with a second-order Godunov code.

We generalize the results for total circulation on non-planar (sinusoidal and circular) interfaces. For the circular bubble case, we introduce a ‘near-normality’ ansatz and obtain a model for total circulation on the bubble surface that agrees well with results of direct numerical simulations. A comparison with other models in the literature is presented.

Type
Research Article
Copyright
© 1994 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

Abd-El-Fattah, A. M. & Henderson, L. F. 1978 Shock waves at a fast-slow gas interface. J. Fluid Mech. 86, 1532.Google Scholar
Arnett, W. D., Bahcall, J. N., Kirshner, R. P. & Woosley, S. E. 1989 Supernova 1987 A. Ann. Rev. Astron. Astrophys. 27, 629.Google Scholar
Bitz, F. & Zabusky, N. J. 1990 David and “Visiometrics”: visualizing, diagnosing and quantifying evolving amorphous objects. Comput. Phys. 4, 603614.Google Scholar
Colella, P. 1985 A direct Eulerian MUSCL scheme for gas dynamics. SIAM J. Sci. Stat. Comput. 6, 104117.Google Scholar
Grove, J. 1989 The interaction of shock waves with fluid interfaces. Adv. Appl. Maths, 10, 201227.Google Scholar
Haas, J. F. & Sturtevant, B. 1987 Interaction of weak shock waves with cylindrical and spherical gas inhomogeneities. J. Fluid Mech. 181, 4176.Google Scholar
Hawley, J. F. & Zabusky, N. J. 1989 Vortex paradigm for shock-accelerated density-stratified interfaces. Phys. Rev. Lett. 63, 12411244.Google Scholar
Henderson, L. F. 1966 The refraction of a plane shock wave at a gas interface. J. Fluid Mech. 26, 607637.Google Scholar
Henderson, L. F. 1989 On the refraction of shock waves. J. Fluid Mech. 198, 365386.Google Scholar
Henderson, L. F., Colella, P. & Puckett, E. G. 1991 On the refraction of shock waves at a slow-fast gas interface. J. Fluid Mech. 224, 127.Google Scholar
Henshaw, W. D., Smyth, N. F. & Schwendeman, D. W. 1986 Numerical shock propagation using geometrical shock dynamics. J. Fluid Mech. 181, 519545.Google Scholar
Jahn, R. G. 1956 The refraction of shock waves at a gaseous interface. J. Fluid Mech. 1, 457489.Google Scholar
Lindl, D. L., McCrory, R. L. & Campbell, E. M. 1992 Progress toward ignition and burn propagation in inertial confinement fusion. Physics Today, pp. 3240, September.
Meshkov, E. E. 1969 Instability of a shock wave accelerated interface between two gases. Izv. Akad. Nauk. SSSR, Mekh. Zhidk. Gaza 5, 151. (NASA Tech. Trans. TT-F-13074, 1970.)Google Scholar
Mulder, W., Osher, S. & Sethian, J. A. 1992 Computing interface motion in compressible gas dynamics. J. Comput. Phys., 100, 209228.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. 1983 Theory of vorticity generation by shock wave and flame interactions. Presented at the 9th ICODERS, Poitiers, France, July 3-8.
Richtmyer, R. D. 1960 Taylor instability in shock acceleration of compressible fluids. Commun. Pure Appl. Maths, XIII, 297319.Google Scholar
Rudinger, G. & Sommers, L. M. 1960 Behaviour of small regions of different gases carried in accelerated gas flows. J. Fluid Mech. 7, 161176.Google Scholar
Samtaney, R. 1993 Vorticity in shock-accelerated density-stratified interfaces : An analytical and computational study. PhD thesis, Rutgers University.
Samtaney, R. & Zabusky, N. J. 1992a Circulation and growth rate in Richtmyer-Meshkov instability using shock polar analysis. Bull. Am. Phys. Soc., 37, 1732.Google Scholar
Samtaney, R. & Zabusky, N. J. 1992b Visiometrics and reduced models for vorticity deposition in shock interactions with heavy cylindrical bubbles. Caip Tech. Rep. 153, Rutgers University.
Samtaney, R. & Zabusky, N. J. 1993 On shock polar analysis and analytical expressions for vorticity deposition in shock-accelerated density-stratified interfaces. Phys. Fluids A 5, 12851287.Google Scholar
Schwendeman, D. W. 1988 Numerical shock propagation in non-uniform media. J. Fluid Mech. 188, 383410.Google Scholar
Silver, D. & Zabusky, N. J. 1992 Quantifying visualizations for reduced modeling in nonlinear science: Extracting structures from data sets. J. Visual Commun. Image Representation 4, 4661.Google Scholar
Smoller, J. 1982 Shock Waves and Reaction-Diffusion Equations. Springer.
Strang, G. 1968 On the construction and comparison of difference schemes. SIAM J. Numer. Anal. 5, 506517.Google Scholar
Sturtevant, B. 1985 Rayleigh-Taylor instability in compressible fluids. Caltech Report. Unpublished.
Van Leer, B. 1977 Towards the ultimate conservative scheme IV: A new approach to numerical convection. J. Comput. Phys. 23, 276299.Google Scholar
Winkler, K.-H., Chalmers, J. W., Hodson, S. W., Woodward, P. R & Zabusky, N. J. 1987 A numerical laboratory. Physics Today 40(10), 2837.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, X., Chern, I.-L., Zabusky, N. J., Samtaney, R. & Hawley, J. F. 1992 Vorticity generation and evolution in shock-accelerated density-stratified interfaces. Phys. Fluids A., 4, 15311540.Google Scholar
Zabusky, N. J., Samtaney, R., Yang, X., Chern, I.-L. & Hawley, J. F. 1992 Vorticity deposition, evolution and mixing for shocked density-stratified interfaces and bubbles. In Shock Waves., (ed. K. Takayama). Proc. 18th Intl. Symp. on Shock Waves, Sendai, Japan. Springer Verlag., July 21–26. Springer.