EMERGENCY BURNING OF SOLID ROCKET PROPELLANT: DAMAGE RISK ASSESSMENT TO PEOPLE IN THE WORKPLACE

M. Biliaiev, O. Berlov, V. Biliaieva, V. Kozachyna, I. Kalashnikov
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Abstract

Purpose. This work includes the development of a computer model to calculate the risk of thermal damage to people in the shop in case of emergency burning of solid rocket propellant. Methodology. To calculate the temperature field in the shop in order to determine the zones of thermal damage to workers in the building, the equation expressing the law of energy conservation was used. Based on this modeling equation, the temperature field in the shop is calculated in the presence of a source of heat emission – burning solid rocket propellant. To calculate the velocity field of air flow in the shop, taking into account the location of obstacles in the path of heat wave propagation, we used the model of vortex-free air motion – the equation of the velocity potential. A two-step finite difference scheme of conditional approximation is used to numerically solve the equation for the velocity potential. A difference splitting scheme was used to numerically solve the energy equation. At the first stage of construction of the difference splitting scheme of the two-dimensional energy equation into the system of one-dimensional equations is performed. Each one-dimensional equation allows you to calculate the temperature change in one coordinate direction. The point-to-point computation scheme is used to determine the temperature. When conducting a computational experiment, the air exchange in the building is taken into account. The risk assessment of thermal damage to personnel in the building is performed for different probabilities of the place of emergency combustion of solid rocket propellant. Findings . Using numerical model prediction of the potential risk areas of thermal damage to staff in the shop for a variety of emergency situations was performed. Originality . A computer model for rapid assessment of the potential risk of damage to people in the shop in case of emergency burning of solid rocket propellant was constructed. Practical value . The authors developed a code that allows you to quickly simulate the temperature fields formation in the shop in case of emergency burning of solid rocket propellant and to identify potential areas of thermal damages to workers based on this information. The developed computer program can be used to assess the risk of thermal damage in the chemical industry in case of emergency.
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固体火箭推进剂的应急燃烧:对工作场所人员的损害风险评估
目的。这项工作包括开发一个计算机模型,以计算在固体火箭推进剂紧急燃烧情况下车间人员的热损伤风险。方法。为了计算车间内的温度场,以确定建筑物内工作人员的热损伤区域,采用了表达能量守恒定律的方程。在此基础上,计算了在固体火箭推进剂燃烧热源存在的情况下,车间内的温度场。为了计算车间内的气流速度场,考虑到热浪传播路径上障碍物的位置,我们采用了无涡空气运动模型——速度势方程。采用条件逼近的两步有限差分格式对速度势方程进行了数值求解。采用差分分裂格式对能量方程进行数值求解。首先,将二维能量方程的差分分割格式构造为一维方程组。每个一维方程都允许你计算一个坐标方向上的温度变化。温度的确定采用点对点计算方案。在进行计算实验时,考虑了建筑物内的空气交换。针对固体火箭推进剂紧急燃烧地点的不同概率,进行了建筑物人员热损伤风险评估。发现。利用数值模型对各种紧急情况下车间工作人员热损伤的潜在危险区域进行了预测。创意。建立了固体火箭推进剂紧急燃烧对车间人员潜在伤害风险快速评估的计算机模型。实用价值。作者开发了一个代码,允许您在紧急燃烧固体火箭推进剂的情况下快速模拟车间中的温度场形成,并根据该信息识别对工人造成热损害的潜在区域。所开发的计算机程序可用于紧急情况下化学工业的热损伤风险评估。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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