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Vol 54, No 4 (2018)

Article

Self-Ignition Model of a Hydrogen Air Mixture

Shults O.V.

Abstract

A numerical analysis of self-ignition of a hydrogen–air–water vapor mixture at different initial pressures is carried out. The results of this analysis are used to make a shortened list of reactions that make the largest contribution to process rate during induction. A simplified analytical description of the system state before self-ignition, which makes it possible to calculate the thermal power and adiabatic heating rate of the system, is presented. A method for estimating the self-ignition limits from the adiabatic heating rate of the mixture is described.

Combustion, Explosion, and Shock Waves. 2018;54(4):385-392
pages 385-392 views

On the Flammability Limit

Zamashchikov V.V.

Abstract

The upper flammability limit of ethane–air and ethane–oxygen mixtures was determined experimentally for various initial temperatures and pressures. In the experiments, the upper flammability limit increased with increasing initial temperature and pressure, which is consistent with literature data. The limit was determined in a closed vessel with central ignition. The obtained limit corresponds to the quenching of the flame propagating downward after its rise under the action of the Archimedes force.

Combustion, Explosion, and Shock Waves. 2018;54(4):393-397
pages 393-397 views

Maximum Pressure during Flame Propagation in a Closed Vessel Partially Filled with a Porous Medium

Kozlov Y.V., Zamashchikov V.V., Korzhavin A.A., Senachin P.K.

Abstract

Flame propagation in a closed vessel containing a stoichiometric propane–air mixture and partially filled with a porous medium was studied experimentally. The porous medium consisted of steel balls of diameter 3.2 and 6 mm and ceramic balls of diameter 6 mm. An experimental dependence of the maximum pressure during flame propagation in the vessel on the degree of filling of the vessel with the porous medium was obtained. Theoretical estimates of the pressure were made, which were in satisfactory agreement with the experimental data. The estimates closest to the data of the experiment are based on the assumption that the gas burns adiabatically in free space and is isothermally compressed in the porous medium. The influence of heat losses from the gas into the porous medium and the walls of the vessel on the maximum pressure was analyzed.

Combustion, Explosion, and Shock Waves. 2018;54(4):398-408
pages 398-408 views

Ignition Delay Time for Hydrogen–Silane–Air Mixtures at Low Temperatures

Tropin D.A., Fedorov A.V., Bochenkov E.S.

Abstract

A modified physicomathematical model of ignition of hydrogen–silane–air mixtures is applied to calculate the ignition delay time for these mixtures at low initial temperatures (300–900 K) and pressures (0.4–1 atm) of the mixture. It is shown that the diagram of the ignition delay time as a function of temperature contains a region of the so-called negative temperature coefficient. The influence of the pressure in the mixture and of the silane fraction on the length of this region is studied. It is found that an increase in both factors (silane concentration and pressure in the mixture) leads to an increase in the length of the negative temperature coefficient region.

Combustion, Explosion, and Shock Waves. 2018;54(4):409-416
pages 409-416 views

Effect of Shell Material on the Detonation of an Explosive Charge

Balagansky I.A., Vinogradov A.V., Merzhievsky L.A., Matrosov A.D., Stadnichenko I.A.

Abstract

The effect of shell material (copper and silicon carbide) on the detonation of a cylindrical explosive charge was analyzed. The wave patterns in the detonation products and the shells are substantially different, which is due to different sound velocities and the rapid destruction of the ceramic under explosive loading. The wave pattern at the explosive/ceramic interface was found to be affected by desensitization of the explosive due to its loading by an advancing wave from the shell side, resulting in a decrease in pressure, blurring of the detonation front, and an increase in particle velocity. Throughout the process, there is a continuous increase in the time of explosive decomposition near the interface between the explosive and the ceramic shell. An extended region with a constant pressure close to the Chapman–Jouguet pressure was observed on the axis of symmetry behind the detonation front of the explosive charge in the ceramic shell.

Combustion, Explosion, and Shock Waves. 2018;54(4):502-510
pages 502-510 views

Acceleration Ability of Emulsion Explosives

Yunoshev A.S., Plastinin A.V., Rafeichik S.I., Voronin M.S.

Abstract

The acceleration ability of an emulsion explosive sensitized with Expancel polymer microballoons and having an initial density of 0.193–1.2 g/cm3 was measured using the end acceleration method and the method of acceleration of a cylindrical shell. The results were compared with those obtained for 79/21 AN/TNT and with the results of ANSYS AUTODYN simulation.

Combustion, Explosion, and Shock Waves. 2018;54(4):496-501
pages 496-501 views

Few-Parameter Equation of State of Copper

Gilev S.D.

Abstract

A few-parameter equation of state in the Mie–Grüneisen form is proposed to describe shock compression of condensed matter. The equation is based on a postulated dependence of the Grüneisen coefficient on the specific volume and temperature Γ(V, T), which provides a qualitative description of compression of metal samples in strong shock waves. The curve of cold compression is found on the basis of the dependence Γ(V, T) with the use of a generalized formula for the Grüneisen function. Heat-induced oscillations of the crystal lattice are described in the Debye approximation. The resultant Grüneisen function has two free parameters. The values of other coefficients of the equation of state are determined from the reference data for matter under normal conditions and also from limiting values under extreme conditions. The model is tested by an example of copper. The derived equation of state describes the cold compression curve, normal isotherm, shock compressibility, as well as the copper unloading curves in density, pressure, and internal energy ranges for which experimental data are available. The thermodynamic characteristics of copper (isentropic modulus of volume compression, velocity of sound, Debye temperature, specific heat, linear expansion coefficient, and melting temperature) are calculated. Comparisons with available experimental data show that the proposed model, despite its simplicity, ensures a consistent description of a large array of experimental data in the region of high energy densities.

Combustion, Explosion, and Shock Waves. 2018;54(4):482-495
pages 482-495 views

Continuous Detonation of Methane/Hydrogen–Air Mixtures in an Annular Cylindrical Combustor

Bykovskii F.A., Zhdan S.A., Vedernikov E.F.

Abstract

Regimes of continuous detonation of methane/hydrogen–air mixtures in spin and opposing transverse detonation waves are obtained for the first time in a flow-type annular cylindrical combustor 503 mm in diameter. A two-component (methane/hydrogen) fuel with the H2 mass fractions of 1/9 to 1/2 in the range of specific flow rates of the mixture from 64 to 1310 kg/(s ·m2) and the fuel-to-air equivalence ratio ϕ = 0.78–1.56 is considered. In methane/hydrogen–air mixtures with two compositions of the fuel (CH4 + 8H2 and CH4 + 4H2), one-wave and two-wave regimes of continuous spin detonation are obtained; the frequency of rotation of transverse detonation waves is 0.56–1.66 kHz at ϕ = 0.78–1.02. For the fuel compositions CH4 + 2H2 and CH4 + 1.5H2, continuous multifront detonation with two opposing transverse detonation waves rotating with the frequency of 0.86–1.34 kHz at ϕ = 1.0–1.23 is obtained. For the CH4 + H2 + air mixture, both combustion in the chamber and continuous spin detonation outside the combustor with transverse detonation waves rotating with the frequency of 1.01–1.1 kHz are observed. The lean limits of continuous detonation are obtained in terms of the specific flow rate of the mixture: 64, 100, 200, and 790 kg/(s · m2) for the fuel compositions CH4 + 8H2, CH4 + 4H2, CH4 + 2H2, and CH4 + 1.5H2, respectively, for the mass fraction of hydrogen in the methane/hydrogen fuel of ≈0.16. Violation of regularity of the continuous detonation wave structure and the wave velocity with a decrease in the fraction of hydrogen in the two-component fuel is detected.

Combustion, Explosion, and Shock Waves. 2018;54(4):472-481
pages 472-481 views

Heating of Energetic Materials by Continuous-Wave Near-IR Laser Radiation

Bachurin L.V., Kolesov V.I., Konovalov A.N., Ul’yanov V.A., Yudin N.V.

Abstract

The heating of energetic materials by the radiation of fiber-coupled continuously-pumped lasers at near IR-wavelengths of 0.98, 1.56, and 1.94 μm was studied. Samples of pressed secondary explosives and loose gunpowder were used. The length of the linear portion of the temperature rise and the rate of its rise immediately after exposure to laser radiation were measured. It was established that the rate of temperature rise at the initial time was proportional to the laser radiation power aP. For a 600 μm diameter of the laser beam emerging from the fiber, the coefficient of proportionality a for secondary explosives was 6–250 K/(s · W) at a wavelength of 0.98 μm and 40–2000 K/(s · W) at wavelengths of 1.56 and 1.94 μm. For gunpowder, a = 7000–15 000 K/(s · W), which is an order of magnitude or more higher than that for most of the secondary explosives we studied. The possibility of increasing the efficiency of laser heating of secondary explosives by applying an absorbing thin film on the surface of the samples was studied. The heating dynamics and the initial stage of ignition of energetic materials by laser radiation were investigated.

Combustion, Explosion, and Shock Waves. 2018;54(4):461-471
pages 461-471 views

Comparative Analysis of Boron Powders Obtained by Various Methods. I. Microstructure and Oxidation Parameters during Heating

Pivkina A.N., Muravyev N.V., Monogarov K.A., Meerov D.B., Fomenkov I.V., Skryleva E.A., Presnyakov M.Y., Vasiliev A.L., Shishov N.I., Milekhin Y.M.

Abstract

This paper describes a study of boron powders and powder compounds, obtained by various methods, including metallothermal, electrolytic, and borane cracking methods. The crystal state, particle size and microstructure, presence and composition of impurities, and chemical composition of the oxide layer of boron particles are profoundly investigated. The effects of the above-mentioned characteristics on the particle oxidation parameters during heating with a constant rate are analyzed. The determining influence of chemical composition of the particle surface layer on the initial temperature of their intense oxidation is established. It is shown that the maximum increase in the mass and heat release value during oxidation of the boron powders is almost independent of microstructural features, crystal state, and chemical composition of and oxide layer thickness of the particles, and cannot serve as indicators of completeness of boron oxidation during heating.

Combustion, Explosion, and Shock Waves. 2018;54(4):450-460
pages 450-460 views

Diffusion Model of Combustion of Large Boron Particles

Ermolaev G.V., Zaitsev A.V.

Abstract

Owing to its high mass and volume heats of combustion, boron is a promising component of solid propellants for air-breathing engines. Its application is limited by difficulties of organizing high-efficiency combustion. Experimental investigations of combustion of individual boron particles demonstrate a large number of unique features, which are not typical for other materials: variable ignition temperature, two stages of combustion, and drastic reduction of the burning rate for particles with sizes of several micrometers or smaller. Models that cover the entire range of temperatures, concentrations, and particle sizes are physically non-obvious, can be hardly reproduced, and do not provide the accuracy needed for solving practical problems. In this paper, we propose a simple diffusion model of combustion, which ensures an adequate description of combustion of boron particles 34.5 and 44.2 μm in size at temperatures above 2240 K.

Combustion, Explosion, and Shock Waves. 2018;54(4):442-449
pages 442-449 views

Effect of a NiO Additive on Interaction in a Ni–Al–W System in Self-Propagating High-Temperature Synthesis

Shchukin A.S., Sytschev A.E.

Abstract

An effect of a NiO additive on the combustion and structure formation in a Ni–Al–W system in self-propagating high-temperature synthesis (SHS) is under study. The stages of the combustion of compositions containing a NiO high-energy additive are shown. The interaction of W particles with Ni–Al melts during SHS results in the formation of globular decoration of particles on the basis of solid solutions of tungsten on the particle surface. This effect is observed only in compositions with an equimolar mixture of Ni–Al. With an NiO additive content in the initial sample more than 1 at.%, the globular decoration on the unreacted W particle surface does not occur. This effect can be associated with changes in the combustion temperature, deviation of the NiAl phase in the direction of a larger content of Ni, and the influence of oxide phases on diffusion processes.

Combustion, Explosion, and Shock Waves. 2018;54(4):433-441
pages 433-441 views

Synthesis of Aluminum Diboride by Thermal Explosion in Mechanically Activated Mixtures of Initial Reactants

Korchagin M.A., Gavrilov A.I., Bokhonov B.B., Bulina N.V., Zarko V.E.

Abstract

Single-phase aluminum diboride was obtained by thermal explosion of an aluminum–boron mixture mechanically activated in a planetary ball mill. The additional mechanical treatment of the products of thermal explosion was found to reduce the coherent scattering area size of AlB2 to nanometer values. The results of x-ray phase and electron microscopy of the mechanocomposites and products of thermal explosion are presented.

Combustion, Explosion, and Shock Waves. 2018;54(4):424-432
pages 424-432 views

Rayleigh–Benard Convection in a Chemically Equilibrium Gas Containing Chemically Inert Microparticles

Palymskiy I.B., Fomin P.A.

Abstract

A physicomathematical model of the Rayleigh–Benard convection in a chemically equilibrium gas containing chemically inert microparticles (Al2O3) is proposed. A linear analysis of convection in the Boussinesq approximation is performed. It is shown that addition of chemically inert microparticles increases the critical value of the Rayleigh number and stability of the convective process. The possibility of using chemically inert microparticles for controlling convection in a chemically reacting gas is demonstrated by an example of a chemically equilibrium gas.

Combustion, Explosion, and Shock Waves. 2018;54(4):417-423
pages 417-423 views

Erratum

Erratum to: “Natural Buoyant Turbulent Diffusion Flame near a Vertical Surface”

Markus E.S., Kuznetsov E.A., Snegirev A.Y.

Abstract

In the original publication, the title was misspelled. It should read “Buoyant Turbulent Diffusion Flame near a Vertical Surface ” instead of “Natural Buoyant Turbulent Diffusion Flame near a Vertical Surface.”

It should also read “buoyant turbulent diffusion flame” instead of “natural buoyant turbulent diffusion flame” everywhere else in the text and “the upward flame spread rate” instead of “the velocity of the upward flame spread rate” in the abstract.

The original Russian text was translated by the journal.

Combustion, Explosion, and Shock Waves. 2018;54(4):511-511
pages 511-511 views