Abstract
The propagation of detonations in layers of reactive gas bounded by inert gas is simulated computationally in both homogeneous and inhomogeneous systems described by the two-dimensional Euler equations with the energy release governed by an Arrhenius rate equation. The thickness of the reactive layer is varied and the detonation velocity is recorded as the layer thickness approaches the critical value necessary for successful propagation. In homogeneous systems, as activation energy is increased, the detonation wave exhibits increasingly irregular cellular structure characteristic of the inherent multidimensional instability. The critical layer thickness necessary to observe successful propagation increases rapidly, by a factor of five, as the activation energy is increased from \(E_\mathrm{a}/RT_0 = 20\)–30; propagation could not be observed at higher activation energies due to computational limitations. For simulations of inhomogeneous systems, the source energy is concentrated into randomly positioned squares of reactive medium embedded in inert gas; this discretization is done in such a way that the average energy content and the theoretical Chapman–Jouguet (CJ) speed remain the same. In the limit of highly discrete systems with layer thicknesses much greater than critical, velocities greater than the CJ speed are obtained, consistent with our prior results in effectively infinite width systems. In the limit of highly discretized systems wherein energy is concentrated into pockets representing 10% or less of the area of the reactive layer, the detonation is able to propagate in layers much thinner (by an order of magnitude) than the equivalent homogeneous system. The critical layer thickness increases only gradually as the activation energy is increased from \(E_\mathrm{a}/R T_0 = 20{-}55\), a behavior that is in sharp contrast to the homogeneous simulations. The dependence of the detonation velocity on layer thickness and the critical layer thickness is remarkably well described by a front curvature model derived from the classic, ZND-based model of Wood and Kirkwood. The results of discrete sources are discussed as a conceptual link to the behavior that is experimentally observed in cellular detonations with highly irregular cellular structure in which intense turbulent burning rapidly consumes detached pockets behind the main shock front. The fact that highly discrete systems are well described by classical, curvature-based mechanisms is offered as a possible explanation as to why curvature-based models are successful in describing heterogeneous, condensed-phase explosives.
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Notes
By laminar, we mean the wave propagates in a layer-by-layer fashion.
Note that, for the most discrete case (\(L = 10\) and \(\varGamma = 0.01\)) with \(E_\mathrm {a} = 10\) shown in Fig. 6a, the resulting wave speed at an infinite reactive layer thickness does not reach the one-dimensional, highly discrete limit. This result can be attributed to the fact that, for such a low activation energy, the time scale of source energy release (\(t_\mathrm {r}\)) is still relatively long, approximately equal to the shock transit time (\(t_\mathrm {s}\)) from one source to the next. As shown in Fig. 9 of Ref. [22], for the cases where the energy release and shock transit time scales are approximately equal, i.e., \(\tau _\mathrm {c} = t_\mathrm {r}/t_\mathrm {s} \approx 1\), the resulting wave speed is only about 2–\(3\%\) greater than the CJ value, which is consistent with the current results with \(E_\mathrm {a} = 10\) at \(h = \infty \).
References
Wood, W., Kirkwood, J.: Diameter effect in condensed explosives. The relation between velocity and radius of curvature of the detonation wave. J. Chem. Phys. 22(11), 1920 (1954). https://doi.org/10.1063/1.1739940
Fay, J.: Two-dimensional gaseous detonations: velocity deficit. Phys. Fluids 2(3), 283 (1959). https://doi.org/10.1063/1.1705924
Fickett, W., Davis, W.: Detonation: Theory and Experiment. Dover, New York (1979)
Higgins, A.: Steady one-dimensional detonations. In: Zhang, F. (ed.) Detonation Dynamics, Shock Waves Science and Technology Library, vol. 6, pp. 33–105. Springer, Berlin (2012). https://doi.org/10.1007/978-3-642-22967-1_2
Radulescu, M., Lee, J.: The failure mechanism of gaseous detonations: experiments in porous wall tubes. Combust. Flame 131(1–2), 29–46 (2002). https://doi.org/10.1016/S0010-2180(02)00390-5
Radulescu, M.: The propagation and failure mechanism of gaseous detonations: experiments in porous-walled tubes. Ph.D. Thesis, McGill University (2003)
Radulescu, M., Borzou, B.: Dynamics of detonations with a constant mean flow divergence. J. Fluid Mech. 845, 346–377 (2018). https://doi.org/10.1017/jfm.2018.244
Radulescu, M.: A detonation paradox: why inviscid detonation simulations predict the incorrect trend for the role of instability in gaseous cellular detonations? Combust. Flame 195, 151–162 (2018). https://doi.org/10.1016/j.combustflame.2018.05.002
Oran, E., Boris, J., Young, T., Flanigan, M., Burks, T., Picone, M.: Numerical simulations of detonations in hydrogen–air and methane–air mixtures. Symp. (Int.) Combust. 18(1), 1641–1649 (1981). https://doi.org/10.1016/S0082-0784(81)80168-3
Oran, E., Young, T., Boris, J., Picone, J., Edwards, D.: A study of detonation structure: the formation of unreacted gas pockets. Symp. (Int.) Combust. 19(1), 573–582 (1982). https://doi.org/10.1016/S0082-0784(82)80231-2
Reynaud, M., Virot, F., Chinnayya, A.: A computational study of the interaction of gaseous detonations with a compressible layer. Phys. Fluids 29(5), 056101 (2017). https://doi.org/10.1063/1.4982659
Reynaud, M.: Numerical study of detonation confined by an inert gas. Theses, ISAE-ENSMA École Nationale Supérieure de Mécanique et d’Aérotechique—Poitiers (2017)
Radulescu, M., Sharpe, G., Lee, J., Kiyanda, C., Higgins, A., Hanson, R.: The ignition mechanism in irregular structure gaseous detonations. Proc. Combust. Inst. 30(2), 1859–1867 (2005). https://doi.org/10.1016/j.proci.2004.08.047
Radulescu, M., Sharpe, G., Law, C., Lee, J.: The hydrodynamic structure of unstable cellular detonations. J. Fluid Mech. 580, 31–81 (2007). https://doi.org/10.1017/S0022112007005046
Maxwell, B., Bhattacharjee, R., Lau-Chapdelaine, S., Falle, S., Sharpe, G., Radulescu, M.: Influence of turbulent fluctuations on detonation propagation. J. Fluid Mech. 818, 646–696 (2017). https://doi.org/10.1017/jfm.2017.145
Pintgen, F., Eckett, C., Austin, J., Shepherd, J.: Direct observations of reaction zone structure in propagating detonations. Combust. Flame 133(3), 211–229 (2003). https://doi.org/10.1016/S0010-2180(02)00458-3
Austin, J., Pintgen, F., Shepherd, J.: Reaction zones in highly unstable detonations. Proc. Combust. Inst. 30(2), 1849–1857 (2005). https://doi.org/10.1016/j.proci.2004.08.157
Shepherd, J.: Detonation in gases. Proc. Combust. Inst. 32(1), 83–98 (2009). https://doi.org/10.1016/j.proci.2008.08.006
Kiyanda, C., Higgins, A.: Photographic investigation into the mechanism of combustion in irregular detonation waves. Shock Waves 23(2), 115–130 (2013). https://doi.org/10.1007/s00193-012-0413-8
Mi, X., Higgins, A.: Influence of discrete sources on detonation propagation in a Burgers equation analog system. Phys. Rev. E 91, 053014 (2015). https://doi.org/10.1103/PhysRevE.91.053014
Mi, X., Timofeev, E., Higgins, A.: Effect of spatial discretization of energy on detonation wave propagation. J. Fluid Mech. 817, 306 (2017). https://doi.org/10.1017/jfm.2017.81
Mi, X., Higgins, A., Ng, H., Kiyanda, C., Nikiforakis, N.: Propagation of gaseous detonation waves in a spatially inhomogeneous reactive medium. Phys. Rev. Fluids 2(5), 053201 (2017). https://doi.org/10.1103/PhysRevFluids.2.053201
Mi, X.: Detonation in spatially inhomogeneous media. Ph.D. Thesis, McGill University (2018)
Sommers, W., Morrison, R.: Simulation of condensed-explosive detonation phenomena with gases. Phys. Fluids 5(3), 241 (1962). https://doi.org/10.1063/1.1706602
Dabora, E., Nicholls, J., Morrison, R.: The influence of a compressible boundary on the propagation of gaseous detonations. Symp. (Int.) Combust. 10(1), 817–830 (1965). https://doi.org/10.1016/S0082-0784(65)80225-9
Dabora, E., Nicholls, J., Sichel, M.: The interaction process between gaseous detonation waves and inert gaseous boundaries: final report. Technical Report 05170-3-F, The University of Michigan, Aircraft Propulsion Laboratory (1965)
Murray, S., Lee, J.: The influence of yielding confinement on large-scale ethylene–air detonations. Prog. Astronaut. Aeronaut. 94, 80–103 (1984). https://doi.org/10.2514/5.9781600865695.0080.0103
Murray, S., Lee, J.: The influence of physical boundaries on gaseous detonation waves. Prog. Astronaut. Aeronaut. 106, 329–355 (1986). https://doi.org/10.2514/5.9781600865800.0329.0355
Vasil’ev, A., Zak, D.: Detonation of gas jets. Combust. Explos. Shock 22, 463–468 (1986). https://doi.org/10.1007/BF00862893
Borisov, A., Khomic, S., Mikhalkin, V.: Detonation of unconfined and semiconfined charges of gaseous mixtures. Prog. Astronaut. Aeronaut. 133, 118–132 (1991). https://doi.org/10.2514/5.9781600866067.0118.0132
Rudy, W., Kuznetsov, M., Porowski, R., Teodorczyk, A., Grune, J., Sempert, K.: Critical conditions of hydrogen–air detonation in partially confined geometry. Proc. Combust. Inst. 34(2), 1965–1972 (2013). https://doi.org/10.1016/j.proci.2012.07.019
Rudy, W., Zbikowski, M., Teodorczyk, A.: Detonations in hydrogen–methane–air mixtures in semi confined flat channels. Energy 116, 1479–1483 (2016). https://doi.org/10.1016/j.energy.2016.06.001
Rudy, W., Dziubanii, K., Zbikowski, M., Teodorczyk, A.: Experimental determination of critical conditions for hydrogen–air detonation propagation in partially confined geometry. Int. J. Hydrog. Energy 42(11), 7366–7373 (2017). https://doi.org/10.1016/j.ijhydene.2016.04.056
Grune, J., Sempert, K., Friedrich, A., Kuznetsov, M., Jordan, T.: Detonation wave propagation in semi-confined layers of hydrogen–air and hydrogen–oxygen mixtures. Int. J. Hydrog. Energy 42(11), 7589–7599 (2017). https://doi.org/10.1016/j.ijhydene.2016.06.055
Houim, R., Fievisohn, R.: The influence of acoustic impedance on gaseous layered detonations bounded by an inert gas. Combust. Flame 179, 185–198 (2017). https://doi.org/10.1016/j.combustflame.2017.02.001
Gaathaug, A., Vaagsaether, K., Bjerketvedt, D.: Detonation failure in stratified layers—the influence of detonation regularity. 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper 908, Boston, MA (2017)
Cho, K., Codoni, J., Rankin, B., Hoke, J., Schauer, F.: Effects of lateral relief of detonation in a thin channel. 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, AIAA Paper 2017-0373 (2017). https://doi.org/10.2514/6.2017-0373
Burr, J., Yu, K.: Detonation wave propagation in cross-flow of discretely spaced reactant jets. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, GA, AIAA Paper 2017-4908 (2017). https://doi.org/10.2514/6.2017-4908
Fujii, J., Kumazawa, Y., Matsuo, A., Nakagami, S., Matsuoka, K., Kasahara, J.: Numerical investigation on detonation velocity in rotating detonation engine chamber. Proc. Combust. Inst. 36(2), 2665 (2017). https://doi.org/10.1016/j.proci.2016.06.155
Ohira, N., Matsuo, A., Kasahara, J., Matsuoka, K.: Numerical investigation on characteristics of a planar detonation wave across layers of burned gas. 26th International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper 994, Boston, MA (2017)
Toro, E.F.: Riemann Solvers and Numerical Methods for Fluid Dynamics, 3rd edn. Springer, Berlin (2009). https://doi.org/10.1007/b79761
Morgan, G.: The Euler equations with a single-step Arrhenius reaction. Master’s Thesis, University of Cambridge (2013)
Kiyanda, C., Morgan, G., Nikiforakis, N., Ng, H.: High resolution GPU-based flow simulation of the gaseous methane–oxygen detonation structure. J. Vis. 18(2), 273–276 (2015). https://doi.org/10.1007/s12650-014-0247-9
Li, J., Mi, X., Higgins, A.: Propagation distance required to reach steady-state detonation velocity in finite-sized charges. In: 15th Symposium (International) on Detonation. Office of Naval Research, Arlington (2014)
Li, J., Mi, X., Higgins, A.: Effect of spatial heterogeneity on near-limit propagation of a pressure-dependent detonation. Proc. Combust. Inst. 35(2), 2025–2032 (2015). https://doi.org/10.1016/j.proci.2014.06.039
Li, J., Mi, X., Higgins, A.: Geometric scaling for a detonation wave governed by a pressure-dependent reaction rate and yielding confinement. Phys. Fluids 27(2), 027102 (2015). https://doi.org/10.1063/1.4907267
Oran, E., Boris, J.: Numerical Simulation of Reactive Flow. Cambridge University Press, Cambridge (2005)
Kasimov, A., Stewart, D.: On the dynamics of self-sustained one-dimensional detonations: a numerical study in the shock-attached frame. Phys. Fluids 16(10), 3566 (2004). https://doi.org/10.1063/1.1776531
Bourlioux, A., Majda, A.: Theoretical and numerical structure for unstable two-dimensional detonations. Combust. Flame 90(3), 211–229 (1992). https://doi.org/10.1016/0010-2180(92)90084-3
Sharpe, G.: Linear stability of idealized detonations. Proc. R. Soc. Lond. A Math. Phys. Eng. Sci. 453(1967), 2603 (1997). https://doi.org/10.1098/rspa.1997.0139
Short, M., Stewart, D.: Cellular detonation stability. Part 1. A normal-mode linear analysis. J. Fluid Mech. 368, 229–262 (1998). https://doi.org/10.1017/S0022112098001682
Sharpe, G., Falle, S.: One-dimensional numerical simulations of idealized detonations. Proc. R. Soc. Lond. A Math. Phys. Eng. Sci. 455(1983), 1203 (1999). https://doi.org/10.1098/rspa.1999.0355
Hwang, P., Fedkiw, R., Merriman, B., Aslam, T., Karagozian, A., Osher, S.: Numerical resolution of pulsating detonation waves. Combust. Theor. Model. 4(3), 217–240 (2000). https://doi.org/10.1088/1364-7830/4/3/301
Sharpe, G.: Transverse waves in numerical simulations of cellular detonations. J. Fluid Mech. 447, 31–51 (2001). https://doi.org/10.1017/S0022112001005535
Ng, H., Higgins, A., Kiyanda, C., Radulescu, M., Lee, J., Bates, K., Nikiforakis, N.: Nonlinear dynamics and chaos analysis of one-dimensional pulsating detonations. Combust. Theor. Model. 9(1), 159–170 (2005). https://doi.org/10.1080/13647830500098357
Henrick, A., Aslam, T., Powers, J.: Simulations of pulsating one-dimensional detonations with true fifth order accuracy. J. Comput. Phys. 213(1), 311–329 (2006). https://doi.org/10.1016/j.jcp.2005.08.013
Ng, H., Zhang, F.: Detonation instability. In: Zhang, F. (ed.) Detonation Dynamics, Shock Waves Science and Technology Library, vol. 6, pp. 107–212. Springer, Berlin (2012). https://doi.org/10.1007/978-3-642-22967-1_3
Eyring, H., Powell, R., Duffy, G., Parlin, R.: The stability of detonation. Chem. Rev. 45(1), 69–181 (1949). https://doi.org/10.1021/cr60140a002
Bdzil, J.: Steady-state two-dimensional detonation. J. Fluid Mech. 108, 195–226 (1981). https://doi.org/10.1017/S0022112081002085
Bdzil, J., Stewart, D.: Modeling two-dimensional detonations with detonation shock dynamics. Phys. Fluids A Fluid Dyn. (1989–1993) 1(7), 1261 (1989). https://doi.org/10.1063/1.857349
Bdzil, J., Stewart, D.: Theory of detonation shock dynamics. In: Zhang, F. (ed.) Detonation Dynamics, Shock Waves Science and Technology Library, vol. 6, pp. 373–453. Springer, Berlin (2012). https://doi.org/10.1007/978-3-642-22967-1_7
Bdzil, J., Aslam, T., Catanach, R., Hill, L., Short, M.: DSD front models: nonideal explosive detonation in ANFO. Technical Report LA-UR-02-4332, Los Alamos National Laboratory (2002)
Lee, J.: On the critical tube diameter. In: Bowen, J. (ed.) Dynamics of Exothermicity, p. 321. Gordon and Breach, Amsterdam (1996)
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The authors thank M. Radulescu, A. Chinnayya, M. Reynaud, and S. Taileb for valuable discussions and critiques of this work. The Tesla K40M processors were acquired under Nvidia’s GPU Grant Program. The Tesla P100 GPU resources were provided by Compute Canada.
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Appendix: Numerical convergence study
Appendix: Numerical convergence study
For two selected values of moderately high activation energy considered, i.e., \(E_\mathrm{a}=20\) and \(E_\mathrm{a}=30\), numerical convergence tests were performed for the homogeneous cases (\(\varGamma =1\)) and the most highly discretized cases (\(\varGamma =0.01\) and \(L=10\)). The convergence study for the resulting critical reactive layer thickness \(h^{*}\) from these cases is shown as the “go” versus “no-go” charts plotted in Figs. 9 and 10.
In Figs. 9, 10, and 11, each symbol represents a case of one or several simulations with a reactive layer thickness h at a numerical resolution in terms of the number of computational cells per the ideal half-reaction-zone length \(l_{1/2}/\varDelta x\). In these figures, a circle \(\circ \) indicates a “go,” i.e., a case resulting in a self-sustained propagation; a cross \(\times \) indicates a “no-go,” i.e., a case of propagation failure. The dashed line indicates the boundary between “go” and “no-go” results that defines the critical thickness \(h^{*}\) as a function of numerical resolution. Considering the stochastic nature of the distribution of reactive sources in a highly inhomogeneous medium, for the near-limit cases, five simulations have been performed for the same value of h. Only if all of these five simulations result in a successful wave propagation over a distance that is more than approximately 150 times the average source spacing L, then the case with the corresponding h is considered as a “go.”
For the homogeneous case with \(E_\mathrm{a}=20\) shown in Fig. 9a, as the numerical resolution was increased from \(l_{1/2}/\varDelta x=10\) to 20, the result of \(h^{*}\) increased by approximately \(9\%\). As the numerical resolution was increased from \(l_{1/2}/\varDelta x=20\) to 30, there was no change greater than \(\pm 4\%\) in the result of \(h^{*}\). For the highly discretized case with \(E_\mathrm{a}=20, \varGamma =0.01\), and \(L=10\) shown in Fig. 9b, there was no change greater than the prescribed average source spacing L in the result of \(h^{*}\) as the resolution was increased from \(l_{1/2}/\varDelta x=5\) to 30. For \(E_\mathrm{a}=30\), the homogeneous case shown in Fig. 10a, as the numerical resolution was increased from \(l_{1/2}/\varDelta x=5\) to 10, the result of \(h^{*}\) increased by approximately \(26\%\). As the numerical resolution was increased from \(l_{1/2}/\varDelta x=10\) to 20, the change in the result of \(h^{*}\) was less than \(\pm 1\%\). As shown in Fig. 10b for the highly discretized case with \(E_\mathrm{a}=30, \varGamma =0.01\), and \(L=10\), there was no change greater than the prescribed average source spacing L in the result of \(h^{*}\) as the resolution was increased from \(l_{1/2}/\varDelta x=5\) to 20.
For the homogeneous cases with both \(E_\mathrm{a}=20\) and \(E_\mathrm{a}=30\) as shown in Figs. 9a and 10a, respectively, simulations at a relatively coarse resolution result in a smaller critical thickness. This reduction in \(h^{*}\) could be attributed to the fact that the effect of numerical diffusion becomes more significant when the inviscid Euler equations are solved at coarser resolutions. In a cellular detonation structure that arises from a homogeneous reactive medium, there is a large amount of reactant that is shocked by the weak parts of the leading shock and undergoes a very slow burning process. The efficiency of this slow reaction process can be significantly enhanced by numerical diffusion. Simulations at coarse resolution likely result in an artificially (numerically) enhanced energy release rate and, thus, enables a detonation wave to propagate in a thinner reactive layer.
For the large values of activation energy \(E_\mathrm{a}=40\) and 55, the simulations have been performed only for the highly inhomogeneous cases with \(\varGamma = 0.01\) and \(L=10\). As shown in Fig. 11a for the cases with \(E_\mathrm{a}=40\), simulations at three different resolutions \(l_{1/2}/\varDelta x=10, 20\), and 30 resulted in the same critical thickness. For the cases with the greatest value of activation energy considered in this study \(E_\mathrm{a}=55\), a minimal resolution of \(l_{1/2}/\varDelta x=20\) was required to obtain numerically converged result of \(h^{*}\) as shown in Fig. 11b. Therefore, the results of \(h^{*}\) as a function of \(E_\mathrm{a}\) presented in Fig. 8 were all based on the simulations at a resolution of \(l_{1/2}/\varDelta x=10\) except the data point for the \(E_\mathrm{a}=55\), highly inhomogeneous case, which was performed at a resolution of \(l_{1/2}/\varDelta x=20\).
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Mi, X.C., Higgins, A.J., Kiyanda, C.B. et al. Effect of spatial inhomogeneities on detonation propagation with yielding confinement. Shock Waves 28, 993–1009 (2018). https://doi.org/10.1007/s00193-018-0847-8
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DOI: https://doi.org/10.1007/s00193-018-0847-8