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AIMING AT QUANTIFYING THE DECELERATION OF SHAPED CHARGE JET PARTICLES IN AIR AT LARGE STAND-OFFS

机译:旨在以较大的停留时间减少空气中异形充气射流颗粒的衰减

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Three experiments with two types of small-scale laboratory shaped charges (SC) were doneand analyzed based on the assumption that parameters which influence the deceleration ofSC particles in air at large stand-offs (SO), e.g. the drag coefficient c_D, can be expressed asan average deceleration coefficient. Two velocity-distance data pairs for each particle weregathered by means of flash X-rays at intermediate SO and by high-speed video cameras atlarge SO. From those data, average deceleration coefficients were calculated. The valuesmainly ranged from 17-88 km~(-1), respectively 3-25 km~(-1), for the two different SC types. Theresults were in agreement with estimates based on the aerodynamic properties of basicshaped bodies. With the method and results, safety ranges or residual penetrationperformance of SC particles at large SO can be estimated in laboratory tests.
机译:使用两种类型的小型实验室异型装药(SC)进行了三个实验 并基于以下假设进行分析:影响减速的参数 空气中的SC粒子具有较大的距离(SO),例如阻力系数c_D可以表示为 平均减速系数。每个粒子有两个速度距离数据对 通过中间SO处的闪光X射线和高速摄像机收集 大SO。根据这些数据,计算出平均减速系数。价值 对于两种不同的SC类型,主要范围为17-88 km〜(-1),分别为3-25 km〜(-1)。这 结果与基于基本空气动力学特性的估计值一致 形体。有了方法和结果,安全范围或残留渗透 大型SO中SC颗粒的性能可以通过实验室测试来评估。

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