This study presents a fragility curve to assess explosively induced damage to military vehicle tires based on shock tube experiments.To replicate lateral damage scenarios that may occur in real battlefield environment...This study presents a fragility curve to assess explosively induced damage to military vehicle tires based on shock tube experiments.To replicate lateral damage scenarios that may occur in real battlefield environments involving missile or bomb detonations,extreme overpressure conditions were generated using a shock tube.The influence of explosive charge mass on tire damage was quantitatively evaluated.Experimental results identified two critical failure thresholds:for loss of pressure,the threshold was 354 kPa peak overpressure and 3052 kPa·ms impulse;for rupture,the values were 485 kPa and 4237 kPa-ms,respectively.The same damage profile was reproduced through finite element analysis(FEA),verifying the reliability of the simulation.A Single Degree of Freedom(SDOF)model and Kingery-Bulmash(K-B)chart were employed to generate pressure-impulse data as a function of standoff distance.These data were applied to a finite element tire model using the BLAST ENHANCED keyword in LS-DYNA.The applied peak overpressures were identical to the experimental values with a 24%-27%difference in impulse.The simulation also captured recurring bead rim separation phenomenon,leading to internal pressure loss consistent with high-speed camera observations from the experiments.The resulting fragility curve clearly defines the threshold conditions for tire damage and provides a standardized damage assessment model applicable to various explosive charge masses and stand-off distances.The proposed model offers a quantitative basis for evaluating tire vulnerability,providing foundational reference data for defense applications.Specifically,the findings are expected to serve as a reliable source for weapon effects analysis and target vulnerability assessments involving wheeled military vehicles.展开更多
为满足弹道散布范围大或大口径弹丸的测速场合,提出了一种原向反射式激光光幕测速的方法.采用半导体激光器、柱透镜、中心留有激光出射孔的光敏检测器件和原向反射屏形成大面积光幕探测区,当高速飞行物体穿越激光光幕时,光通量的变化被...为满足弹道散布范围大或大口径弹丸的测速场合,提出了一种原向反射式激光光幕测速的方法.采用半导体激光器、柱透镜、中心留有激光出射孔的光敏检测器件和原向反射屏形成大面积光幕探测区,当高速飞行物体穿越激光光幕时,光通量的变化被光敏管阵列转变为电信号并采集到计算机进行数据处理.提出了玻璃微珠原向反射器的剩余发散角这个重要概念和利用数字CM O S相机对其进行测试的方法和结果.利用有效光幕区为Φ500 mm的激光测速系统对7.62 mm弹丸的速度进行了测试,给出了试验波形和一组测试数据.试验证明:该方法具有可形成的有效光幕区面积大、光路调整简单、成本低、灵敏度高等优点.展开更多
基金part of the Agency for Defense Development(ADD)research project on Weapon lethality/effectiveness analysis technology for material targets and grant funded by the korean goverment(511225-912A03301)。
文摘This study presents a fragility curve to assess explosively induced damage to military vehicle tires based on shock tube experiments.To replicate lateral damage scenarios that may occur in real battlefield environments involving missile or bomb detonations,extreme overpressure conditions were generated using a shock tube.The influence of explosive charge mass on tire damage was quantitatively evaluated.Experimental results identified two critical failure thresholds:for loss of pressure,the threshold was 354 kPa peak overpressure and 3052 kPa·ms impulse;for rupture,the values were 485 kPa and 4237 kPa-ms,respectively.The same damage profile was reproduced through finite element analysis(FEA),verifying the reliability of the simulation.A Single Degree of Freedom(SDOF)model and Kingery-Bulmash(K-B)chart were employed to generate pressure-impulse data as a function of standoff distance.These data were applied to a finite element tire model using the BLAST ENHANCED keyword in LS-DYNA.The applied peak overpressures were identical to the experimental values with a 24%-27%difference in impulse.The simulation also captured recurring bead rim separation phenomenon,leading to internal pressure loss consistent with high-speed camera observations from the experiments.The resulting fragility curve clearly defines the threshold conditions for tire damage and provides a standardized damage assessment model applicable to various explosive charge masses and stand-off distances.The proposed model offers a quantitative basis for evaluating tire vulnerability,providing foundational reference data for defense applications.Specifically,the findings are expected to serve as a reliable source for weapon effects analysis and target vulnerability assessments involving wheeled military vehicles.
文摘为满足弹道散布范围大或大口径弹丸的测速场合,提出了一种原向反射式激光光幕测速的方法.采用半导体激光器、柱透镜、中心留有激光出射孔的光敏检测器件和原向反射屏形成大面积光幕探测区,当高速飞行物体穿越激光光幕时,光通量的变化被光敏管阵列转变为电信号并采集到计算机进行数据处理.提出了玻璃微珠原向反射器的剩余发散角这个重要概念和利用数字CM O S相机对其进行测试的方法和结果.利用有效光幕区为Φ500 mm的激光测速系统对7.62 mm弹丸的速度进行了测试,给出了试验波形和一组测试数据.试验证明:该方法具有可形成的有效光幕区面积大、光路调整简单、成本低、灵敏度高等优点.
