2008
DOI: 10.1007/s10573-008-0022-0
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Structure and initiation of plane detonation waves in a bidisperse gas suspension of aluminum particles

Abstract: Initiation and propagation of plane waves of heterogeneous detonation in a stoichiometric suspension of two fractions of aluminum particles in oxygen are analyzed numerically. It is found that the detonation is not ideal, and the steady-state part of the shock-wave structure is bounded by an equilibrium frozen sonic point. Initiation criteria depend on the particle-size distribution of the mixture. Initiation by explosive shock waves can lead to formation of unstable two-front structures. Addition of a small a… Show more

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Cited by 18 publications
(11 citation statements)
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“…Detonation in bidisperse suspensions was studied in [9,10]. Based on an analysis of a self-similar solution of nonideal detonation, the possibility of existence of two-front regimes in a bidisperse suspension of monofuel particles was demonstrated in [9].…”
Section: Introductionmentioning
confidence: 99%
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“…Detonation in bidisperse suspensions was studied in [9,10]. Based on an analysis of a self-similar solution of nonideal detonation, the possibility of existence of two-front regimes in a bidisperse suspension of monofuel particles was demonstrated in [9].…”
Section: Introductionmentioning
confidence: 99%
“…Based on an analysis of a self-similar solution of nonideal detonation, the possibility of existence of two-front regimes in a bidisperse suspension of monofuel particles was demonstrated in [9]. The processes of initiation and propagation of plane detonation waves in a bidisperse gas suspension of aluminum particles in oxygen were numerically examined in [10]. Significant differences from monodisperse suspensions were observed, in terms of both the initiation scenario and the structure of steady-state waves.…”
Section: Introductionmentioning
confidence: 99%
“…Fedorov et al [6,[10][11][12][13][14]19]. This criterion was substantiated in [27] when considering the ignition of aluminum particles in a shock wave, taking into account surface oxidation reactions and polymorphic transformations of the oxide.…”
Section: Nanosized Particle Ignition and Combustionmentioning
confidence: 98%
“…According to the data given in [16], the burning time of aluminum particles in a mixture of oxygen and nitrogen in the range 10 nm -100 nm obeys the dependence [6] used in the analysis and numerical modeling of micron particle suspensions [10][11][12][13][14]19], the reaction of reduced kinetics was assumed to be of the Arrhenius type with an activation energy of 32 kJ/mol (half the data for aluminum nanoparticles), thus reflecting the transitional combustion regime.…”
Section: Nanosized Particle Ignition and Combustionmentioning
confidence: 99%
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