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Vol 53, No 6 (2017)

Article

Numerical investigation of the distribution of oxygen atoms in syngas combustion products

Shvartsberg V.M., Bunev V.A., Babkin V.S.

Abstract

The distribution of air oxygen atoms in the oxidation products of rich mixtures of syngas with air in flame and the under autoignition conditions at constant volume has been investigated by numerical simulation using the tracer method. It has been found that in rich mixtures, the oxidation of hydrogen and carbon oxide has a stepwise nature, which is clearly visible in the profiles of the rates of production of H2O and CO2. The observed stepwise nature inevitably results in the heat-release rate occurring in steps. The reaction pathways and the role of the oxygen atom of the CO molecule in the heat release in these flames has been investigated.

Combustion, Explosion, and Shock Waves. 2017;53(6):619-625
pages 619-625 views

Effect of catalytic combustion of hydrogen on the dehydration processes in a membrane reactor. III. calculation of the industrial reactor

Shelepova E.V., Vedyagin A.A., Noskov A.S.

Abstract

This paper describes the mathematical simulation of an industrial membrane reactor for propane dehydrogenation in the thermodynamic coupling with hydrogen combustion (oxidation). Due to the effective removal of hydrogen through a membrane and the heat release as a result of an exothermic reaction, the temperature of the reaction stream at the input could be reduced to 500◦C. The fact that the process is carried out on an industrial-level membrane reactor makes it possible to reach a propane conversion of 75% with a propylene selectivity of 97%, which exceeds the figures obtained per pass in existing industrial devices at higher temperatures.

Combustion, Explosion, and Shock Waves. 2017;53(6):626-633
pages 626-633 views

Performance optimization of a standard-flow hybrid rocket engine

Arkhipov V.A., Bondarchuk S.S., Zhukov A.S., Zolotorev N.N., Perfil’eva K.G.

Abstract

A method for performance optimization of a standard-flow hybrid rocket engine is considered. The method is based on inserting an additional amount of an oxidizer into a solid propellant with a prescribed distribution of the oxidizer mass fraction along the solid propellant charge. An analytical dependence is derived for the oxidizer fraction distribution that ensures uniform combustion and high efficiency of the solid propellant charge.

Combustion, Explosion, and Shock Waves. 2017;53(6):634-640
pages 634-640 views

Determination of the transfer coefficients of natural turbulence occurring near the solid-propellant gasification zone. II. hydrodynamic instability in the presence of cross-flow

Sabdenov K.O., Erzada M.

Abstract

A solution is obtained to the problem of determining the conditions of hydrodynamic stability in the presence of flow of gaseous combustion products over the propellant gasification surface. The cross-flow has a small gradient along the direction of motion. Analysis of the obtained dispersion equation shows that hydrodynamic instability with oscillations develops. The transfer coefficients of natural turbulence are represented as the sum of two terms: the first is responsible for the transfer in the absence of cross-flow, and the second takes into account the enhancement of transport processes in the case of cross-flow. Their dependence on the initial temperature of solid propellant combustion predicts a reduction in the negative erosion effect in accordance with experimental data. Accounting for the relaxation time of the evaporation process has a stabilizing effect. In the limit of strong relaxation, this leads to oscillatory stability (in the absence of crossflow) where the perturbations neither grow nor decay. However, arbitrarily weak cross-flow leads to instability.

Combustion, Explosion, and Shock Waves. 2017;53(6):641-651
pages 641-651 views

Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles

Rashkovskii S.A., Milekhin Y.M., Fedorychev A.V.

Abstract

A mathematical model of combustion of boron particles in a ram-rocket engine is developed. The boron combustion efficiency for one-stage and two-stage injection of air into the afterburning chamber is calculated. It is demonstrated that two-stage injection of air sometimes allows the time of complete combustion of boron particles to be significantly reduced (by a factor of 1.5–3); thus, the fuel combustion efficiency in the ram-rocket engine can be increased. The simulated results are consistent with available experimental data.

Combustion, Explosion, and Shock Waves. 2017;53(6):652-664
pages 652-664 views

Combustion and autowave chemical transformations of a highly exothermic CaCrO4/Al/B mixture

Yukhvid V.I., Gorshkov V.A., Ignat’eva T.I., Semenova V.N., Shchukin A.S., Miloserdov P.A.

Abstract

The combustion of a highly exothermic mixture of calcium chromate with aluminum and boron has been studied. It has been shown that these mixtures are able to burn in a wide range of reactant ratios. The autowave chemical transformation is accompanied by decomposition of calcium chromate, the chemical reaction of the decomposition products with aluminum and boron, the formation of a two-phase melt of the combustion products with its subsequent gravity separation, and crystallization of the layers. The results of the study may be useful for obtaining chromium borides.

Combustion, Explosion, and Shock Waves. 2017;53(6):665-668
pages 665-668 views

Self-propagating high-temperature synthesis in mechanically activated mixtures of boron carbide and titanium

Korchagin M.A., Gavrilov A.I., Zarko V.E., Kiskin A.B., Iordan Y.V., Trushlyakov V.I.

Abstract

Self-propagating high-temperature synthesis in both the modes of both layer-by-layer combustion and dynamic thermal explosion was carried out using preliminary mechanical activation of B4C–Ti powder mixtures in a planetary ball mill. Preliminary mechanical activation conditions of reaction mixtures that provide a reduction in the reaction initiation temperature to 600 ± 20◦C were determined. The reaction products consist of mixtures of TiC and TiB2 with submicron grain size. The results of x-ray diffraction and electron microscopy studies of activated samples and reaction products are presented.

Combustion, Explosion, and Shock Waves. 2017;53(6):669-677
pages 669-677 views

Experimental study of the suppression of flaming combustion and thermal decomposition of model ground and crown forest fires

Volkov R.S., Kuznetsov G.V., Strizhak P.A.

Abstract

This paper presents an experimental study of heat and mass transfer and phase transformations in the suppression of flaming combustion and thermal decomposition of model ground, crown, and mixed forest fires due to local exposure to water. The experiments were carried out with typical combustible forest materials (mixture of leaves, needles, and twigs) and models of trunks and branches of trees. The conditions and characteristics of suppression of the flaming combustion and thermal decomposition of combustible forest materials were determined. It is shown that in the case of crown and mixed fires, local short-term (a few seconds) action of a liquid projectile does not suppress the thermal decomposition of the material (but can only lead to localization of flaming combustion). In the case of ground forest fires, this approach can be efficient with an appropriate choice of the water-irrigated area of the combustion zone and the rate and time of water spraying.

Combustion, Explosion, and Shock Waves. 2017;53(6):678-688
pages 678-688 views

Shock wave distribution in an explosion of an explosive material with plastic filler

Gerasimov S.I., Mikhailov A.L., Trepalov N.A.

Abstract

This paper describes the measurement results for the shock wave propagation during an explosion of an explosive material with plastic filler. The detection is carried out with the help of high-speed analog and digital video cameras. The air shock wave is visualized by means of shadow photography in transmitted light in the zone of separation from expanding explosion products and using a background oriented schlieren method in the far zone. The optical measurements of the air shock wave propagation are used to estimate a maximum pressure in the compression zone at different sections and compared with the data obtained by the pressure gauges. The calculated pressure peaks are in good agreement with the measured ones. The background oriented schlieren method proves to be a useful tool easily introduced in conventional large-scale polygon experiments.

Combustion, Explosion, and Shock Waves. 2017;53(6):689-695
pages 689-695 views

Numerical study of dispersion of a rough dense layer of particles under the action of an expanding shock wave

Khmel’ T.A., Fedorov A.V.

Abstract

Interaction of an expanding shock wave with a layer of particles having a rough surface is considered within the framework of the collisional model of a gas suspension. The influence of roughness on the shape of the contact boundaries in the gas phase and on the boundaries of the cloud of particles is analyzed. The development of the Richtmyer–Meshkov instability is demonstrated. Factors of particle dispersion are determined. Instability evolution is found to increase the amplitude of surface disturbances, and the development of collision dynamics favors smearing of finger-type structures. If the particle motion is essentially random, the pattern of cloud spreading is similar to that observed in experiments.

Combustion, Explosion, and Shock Waves. 2017;53(6):696-704
pages 696-704 views

Mean detonation velocity in poorly mixed gas mixtures

Prokhorov E.S.

Abstract

A method is proposed for calculating the mean velocity of the front of a plane detonation wave in a poorly mixed mixture of a gaseous hydrocarbon fuel and an oxidizer (oxygen or air). It is assumed that the chemical composition of the mixture exhibits periodic fluctuations in the detonation propagation direction, e.g., owing to gas charge stratification. The method is based on analyzing the functional dependence of the ideal (Chapman–Jouguet) detonation velocity on the molar fraction (normalized molar concentration) of the fuel. It is demonstrated that the mean detonation velocity can be appreciably (by 10–15%) smaller than the ideal detonation velocity. A dependence is found, which allows one to estimate the degree of mixing of the gas mixture on the basis of mean detonation velocity measurements.

Combustion, Explosion, and Shock Waves. 2017;53(6):705-710
pages 705-710 views

Energy release in multifront detonation

Vasil’ev A.A., Vasiliev V.A.

Abstract

A method is proposed for determining the energy release in a combustible mixture, which is based on processing the trajectory of the expanding wave from the viewpoint of the strong explosion model. The wave trajectory in the case of critical initiation of multifront detonation in a combustible mixture is compared with the trajectory of a blast wave generated by the same initiator in an inert mixture whose gas-dynamic parameters are equivalent to those of the combustible mixture. The energy release is defined as the difference between the joint energy release of the initiator and combustible mixture in the case of critical initiation and the energy release of the initiator in the case of blast wave excitation in the inert mixture. Results of experimental validation of the method by an example of a stoichiometric acetylene–oxygen mixture are presented. Noticeable deviations of the experimental profile of energy release from available model concepts are observed.

Combustion, Explosion, and Shock Waves. 2017;53(6):711-717
pages 711-717 views

Computer simulation of the structure and electronic and detonation properties of energy materials

Prazyan T.L., Zhuravlev Y.N.

Abstract

Computer modeling is used within the framework of the theory of density functional to determine the physical and chemical properties of a set of energy materials, which correlate with detonation parameters and sensitivity factors. There are two models of prediction of detonation parameters and sensitivity factors formulated for molecules and explosive crystals that satisfactorily correlate with the experimental data.

Combustion, Explosion, and Shock Waves. 2017;53(6):718-723
pages 718-723 views

Laser initiation of mixtures of PETN and aluminum by a deposit

Tarzhanov V.I., Sdobnov V.I., Zinchenko A.D., Pogrebov A.I., Tokarev B.B.

Abstract

The formation of a deposit from mixtures of PETN with fine aluminum under the action of neodymium laser radiation in a free generation mode is studied. This paper also describes the efficiency of a deposit as a means to reduce the energy of laser initiation of mixtures as a function of fineness of PETN, aluminum content in initiated mixtures and deposit, mixture density, and diameter of the laser action region on the explosive. The compositions of mixtures for preparing deposits optimal in composition, which reduce the initiation energy of mixtures of PETN and aluminum down to 3.75 times, are determined. The functioning mechanism of a deposit during laser initiation of mixtures of PETN and aluminum is under discussion.

Combustion, Explosion, and Shock Waves. 2017;53(6):724-729
pages 724-729 views

Detonation temperature of an emulsion explosive with a polymer sensitizer

Bordzilovskii S.A., Karakhanov S.M., Plastinin A.V., Rafeichik S.I., Yunoshev A.S.

Abstract

Dependences of the brightness temperatures of the detonation front and detonation products on detonation pressure were determined in the range of 0.7–9.4 GPa by a pyrometric method. The pressure was varied by changing the initial density of the emulsion explosive in the range of 0.43–1.2 g/cm3. Polymer microballoons were used as sensitizer. The dependence of the brightness temperature in the Chapman–Jouguet plane on detonation pressure was found to be nonmonotonic. In the investigated pressure range, the measured temperature values varied from 2250 to 1830 K. A comparative analysis of the application of polymer and glass microballoons as sensitizers was performed. The obtained experimental data were compared with the calculation results available in the literature.

Combustion, Explosion, and Shock Waves. 2017;53(6):730-737
pages 730-737 views

Detonation velocity of an emulsion explosive sensitized with polymer microballoons

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

Abstract

This paper presents the results of investigation of the detonation velocity of an emulsion explosive sensitized with Expancel polymer microballoons in a wide range of initial density of 0.14–1.33 g/cm3. It is shown that at a density of the emulsion explosive less than 0.4 g/cm3, detonation with an unstable front characteristic of liquid explosives is possible.

Combustion, Explosion, and Shock Waves. 2017;53(6):738-743
pages 738-743 views

Application and properties of nanometric HMX in PBX

Liu J., Hao G., Rong Y., Xiao L., Jiang W., Li F., Jing C., Gao H., Chen T., Ke X.

Abstract

A nanometric HMX-based polymer-bonded explosive (PBX) is prepared by using the solution-water slurry technique. The resultant PBX is composed of 94% of HMX, 5% of fluororubber Viton, and 1% of wax. The properties of the nanometric HMX-based PBX, such as sensitivity and compressive performance, are comprehensively researched. The results show significant improvement for the nanometric HMX-based PBX as compared to the micron-sized HMX-based PBX. The friction sensitivity, impact sensitivity, and shock sensitivity of the nanometric HMX-based PBX are obviously lower by 30, 48, and 24%, respectively. Moreover, the compressive strength and strain of the nanometric HMX-based PBX are significantly higher by 273 and 33%, respectively. Thus, both the safety and mechanical resistibility of the PBX will significantly benefit from using nanometric HMX.

Combustion, Explosion, and Shock Waves. 2017;53(6):744-749
pages 744-749 views