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SOLID PROPELLANT BURN RATE MEASUREMENT IN A MICRO CLOSED BOMB

机译:微封闭炸弹中固体推进剂燃烧率测量

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In the present work experimental data from seven perforated (7PF) JA2 propellantcombustion in a micro closed bomb is presented and the linear burning rate of the JA2propellant is determined. The burn rate measurement is based on a sophisticated lumpedparameter model which accounts among other things for arbitrary cross sectional propellantgeometries with the help of the ICT-Cellular-Combustion-Algorithm (ICCA), pressuredependent thermophysical parameters and heat loss. The model is used to construct avivacity based objective function which depends on the parameters of the empirical law forthe linear burning velocity. With the Nelder-Mead downhill simplex optimization algorithmthe objective function is minimized and the burn rate parameters determined. Thecomparison of the results to published data show that with the new burn rate measurementmethod the linear burning rate can be determined with great accuracy even when only a fewpropellant grains with a total propellant mass of less than 8 g per shot are used.
机译:在本作工作中的实验数据来自七个穿孔(7pf)Ja2推进剂 提出了微闭炸弹中的燃烧和JA2的线性燃烧率 推进剂确定。燃烧速率测量基于复杂的集声 参数模型,用于任意横截面推进剂的其他东西 借助ICT - 细胞燃烧算法(ICCA),压力的几何 依赖热物理参数和热量损失。该模型用于构建一个 基于Vivacity的目标函数,取决于实证法的参数 线性燃烧速度。与Nelder-Mead下坡单纯x优化算法 目标函数最小化并且确定燃烧速率参数。这 将结果与发布数据的比较显示,具有新的烧伤率测量 方法即使只有少数,也可以以极高的准确度确定线性燃烧速率 使用具有每次喷射量小于8g的总推进剂质量的推进剂晶粒。

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