条形挡光片测速的误差分析及修正方法

在利用气垫导轨装置及配件进行的各类实验中,速度作为一个基本的待测量,其准确测量有着重要的意义.通常利用MUJ-6B通用计数器记录不同类型挡光片经过光电门的遮光时间,用游标卡尺测得遮光距离从而得到速度值.本文从光电计时原理分析了使用U形挡光片、计时方式2不会出现系统误差,而使用条形挡光片、计时方式1会出现较大系统误差的原因.我们进一步利用气垫导轨上两弹簧连接滑块做简谐振动模型的理论公式推导出条形挡光片遮光时被光电门"吞掉"的宽度,进而得到了速度的修正公式.此外,通过气垫导轨上的动量守恒实验从另外一个角度验证了速度修正方法的正确性.     

Simulations on the multi-shell target ignition driven by radiation pulse in Z-pinch dynamic hohlraum

We present the first simulation results of a multi-shell target ignition driven by Z-pinch dynamic hohlraum radiation pulse. The radiation pulse is produced with a special Z-pinch dynamic hohlraum configuration, where the hohlraum is composed of a single metal liner, a low-Z plastic foam, and a high-Z metallic foam. The implosion dynamics of a hohlraum and a multi-shell target are investigated separately by the one-dimensional code MULTI-IFE. When the peak drive current is 50 MA, simulations suggest that an x-ray pulse with nearly constant radiation temperature (～ 310 eV) and a duration about 9 ns can be obtained. A small multi-shell target with a radius of 1.35 mm driven by this radiation pulse is able to achieve volumetric ignition with an energy gain (G) about 6.19, where G is the ratio of the yield to the absorbed radiation. Through this research, we better understand the effects of non-uniformities and hydrodynamics instabilities in Z-pinch dynamic hohlraum.