976 resultados para Detonation Velocity


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A simple yet fairly accurate method of calculating the ideal detonation velocity of an organic explosive from a knowledge of the chemical composition alone is proposed. The method is based on the concept that the energetics of a stoichiometrically balanced fuel-oxidizer system is a function of the total oxidizing or reducing valences of the composition. A combination of the valences in the form of Image , where R and P are, respectively, the reducing and oxidizing valences and MW is the molecular weight, has been found to be linearly related to the detonation velocity of the expolosive. The predicting capacity of the method has been found to be superior to other methods in the literature.

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Commercial explosives behave non-ideally in rock blasting. A direct and convenient measure of non-ideality is the detonation velocity. In this study, an alternative model fitted to experimental unconfined detonation velocity data is proposed and the effect of confinement on the detonation velocity is modelled. Unconfined data of several explosives showing various levels of nonideality were successfully modelled. The effect of confinement on detonation velocity was modelled empirically based on field detonation velocity measurements. Confined detonation velocity is a function of the ideal detonation velocity, unconfined detonation velocity at a given blasthole diameter and rock stiffness. For a given explosive and charge diameter, as confinement increases detonation velocity increases. The confinement model is implemented in a simple engineering based non-ideal detonation model. A number of simulations are carried out and analysed to predict the explosive performance parameters for the adopted blasting conditions.

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Este trabalho é realizado no domínio das obras de engenharia, área onde o desmonte de rocha com recurso a explosivos em obras rodoviárias é uma actividade específica e consistiu no acompanhamento e execução de três obras rodoviárias de média e grande dimensão. A necessidade de executar escavações, recorrendo a técnicas de desmonte cuidadoso de contorno, onde o plano de corte do talude final deve obedecer a requisitos de localização, alinhamento, inclinação, estabilidade e também estéticos, acrescendo a isto a necessidade de optimizar os meios envolvidos, obriga a que esta actividade seja encarada de uma forma sistematizada, visando o racional aproveitamento de recursos. A execução desta actividade requer conhecimentos no domínio das técnicas de desmonte de contorno, dos explosivos, do mecanismo de rotura de rochas, da operação de perfuração e da geomecânica dos maciços. A abordagem deste trabalho incide sobre a técnica denominada de pré‐corte e tem como objectivo encontrar uma equação característica que permita relacionar diferentes parâmetros envolvidos nesta actividade. Este objectivo é alcançado recorrendo à correlação entre equações relativas à pressão de detonação, à pressão no furo e ao espaçamento entre furos consecutivos, desenvolvidas por outros autores. Desta forma obteve‐se uma equação que relaciona parâmetros relativos ao maciço rochoso (resistência à tracção), ao explosivo (velocidade de detonação e densidade) e ao diagrama de fogo (concentração de carga – volume de explosivo e comprimento do furo – volume do furo). A comparação entre os valores destes parâmetros obtidos na produção e os obtidos com recurso à equação característica permite concluir que a sua aplicação para execução de futuras obras possibilita uma optimização dos meios envolvidos.

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Pseudomonas putida GG04 and Bacillus SF have been successfully incorporated into an explosive formulation to enhance biotransformation of TNT residues and/or explosives which fail to detonate due to technical faults. The incorporation of the microorganisms into the explosive did not affect the quality of the explosive (5 years storage) in terms of detonation velocity while complete biotransformation of TNT moieties upon transfer in liquid media was observed after 5 days. The incorporated microorganisms reduced TNT sequentially leading to the formation of hydroxylaminodinitrotoluenes (HADNT), 4-amino-2,6-dinitrotoluenes; 2-amino-4,6-dinitrotoluenes, different azoxy compounds; 2,6-diaminonitrotoluenes (2,4-DAMNT) and 2,4-diaminonitrotoluenes (2,6-DAMNT). However, the accumulation of AMDNT and DAMNT (major dead-end metabolites) was effectively prevented by incorporating guaiacol and catechol during the biotransformation process.

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El presente proyecto trata de un análisis de las mediciones de la velocidad de detonación, obtenidas por diferentes métodos y dispositivos. Tiene como objetivo la inter-comparación de los resultados entre diferentes organismos para poder analizar las desviaciones e incertidumbres de las diferentes metodologías de medidas empleadas actualmente. Para ello, se realizaron medidas con dos tipos de explosivos por diferentes métodos y con dispositivos de medida distintos. A partir de esas mediciones y de las propiedades técnicas de los explosivos empleados, se determinó cuáles son los métodos más recomendables para utilizar en cada explosivo, y que dispositivos de medición de la velocidad de detonación más adecuado. ABSTRACT This project is an analysis of the velocity of detonation measurements, obtained by different kind of methods and devices. The aim of work is to compare the results between different laboratories and to be able to analyze the deviations and uncertainties the different measurement methodologies currently used. For that purpose, measurements were made with different explosives, and it was determined which methods and devices are the most suitable for each explosive. From these measurements and the technical features of each explosive used, we established what are the most suitable for each explosive use, and which is the most appropiate device to measure the detonation velocity.

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Damage not only degrades the mechanical properties of explosives, but also influences the shock sensitivity, combustion and even detonation behavior of explosives. The study of impact damage is crucial in the vulnerability evaluation of explosives. A long-pulse low-velocity gas gun with a gas buffer was developed and used to induce impact damage in a hot pressed plastic bonded explosive. Various methods were used to detect and characterize the impact damage of the explosive. The microstructure was examined by use of polarized light microscopy. Fractal analysis of the micrographs was conducted by use of box counting method. The correlation between the fractal dimensions and microstructures was analyzed. Ultrasonic testing was conducted using a pulse through-transmission method to obtain the ultrasonic velocity and ultrasonic attenuation. Spectra analyses were carried out for recorded ultrasonic signals using fast Fourier transform. The correlations between the impact damage and ultrasonic parameters including ultrasonic velocities and attenuation coefficients were also analyzed. To quantitatively assess the impact induced explosive crystal fractures, particle size distribution analyses of explosive crystals were conducted by using a thorough etching technique, in which the explosives samples were soaked in a solution for enough time that the binder was totally removed. Impact induces a large extent of explosive crystal fractures and a large number of microcracks. The ultrasonic velocity decreases and attenuation coefficients increase with the presence of impact damage. Both ultrasonic parameters and fractal dimension can be used to quantitatively assess the impact damage of plastic bonded explosives.

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The performance of combustion driver ignited by multi-spark plugs distributed along axial direction has been analysed and tested. An improved ignition method with three circumferential equidistributed ignitors at main diaphragm has been presented, by which the produced incident shock waves have higher repeatability, and better steadiness in the pressure, temperature and velocity fields of flow behind the incident shock, and thus meets the requirements of aerodynamic experiment. The attachment of a damping section at the end of the driver can eliminate the high reflection pressure produced by detonation wave, and the backward detonation driver can be employed to generate high enthalpy and high density test flow. The incident shock wave produced by this method is well repeated and with weak attenuation. The reflection wave caused by the contracted section at the main diaphragm will weaken the unfavorable effect of rarefaction wave behind the detonation wave, which indicates that the forward detonation driver can be applied in the practice. For incident shock wave of identical strength, the initial pressure of the forward detonation driver is about 1 order of magnitude lower than that of backward detonation.

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We present results for a suite of 14 three-dimensional, high-resolution hydrodynamical simulations of delayed-detonation models of Type Ia supernova (SN Ia) explosions. This model suite comprises the first set of three-dimensional SN Ia simulations with detailed isotopic yield information. As such, it may serve as a data base for Chandrasekhar-mass delayed-detonation model nucleosynthetic yields and for deriving synthetic observables such as spectra and light curves. We employ aphysically motivated, stochastic model based on turbulent velocity fluctuations and fuel density to calculate in situ the deflagration-to-detonation transition probabilities. To obtain different strengths of the deflagration phase and thereby different degrees of pre-expansion, we have chosen a sequence of initial models with 1, 3, 5, 10, 20, 40, 100, 150, 200, 300 and 1600 (two different realizations) ignition kernels in a hydrostatic white dwarf with a central density of 2.9 × 10 g cm, as well as one high central density (5.5 × 10 g cm) and one low central density (1.0 × 10 g cm) rendition of the 100 ignition kernel configuration. For each simulation, we determined detailed nucleosynthetic yields by postprocessing10 tracer particles with a 384 nuclide reaction network. All delayed-detonation models result in explosions unbinding thewhite dwarf, producing a range of 56Ni masses from 0.32 to 1.11M. As a general trend, the models predict that the stableneutron-rich iron-group isotopes are not found at the lowest velocities, but rather at intermediate velocities (~3000×10 000 km s) in a shell surrounding a Ni-rich core. The models further predict relatively low-velocity oxygen and carbon, with typical minimum velocities around 4000 and 10 000 km s, respectively. © 2012 The Authors. Published by Oxford University Press on behalf of the Royal Astronomical Society.