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Study of thermal shock wave in shock-compressed He II induced by gas dynamic shock wave impingement

机译:气体动态冲击波冲击诱导冲击压缩的热冲击波研究

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Strong thermal shock waves induced by the impingement of a gas dynamic shock wave onto a He II free surface in the superfluid shock tube facility were investigated by measuring temperature variation with superconductive temperature sensors and by Schlieren visualization method with an ultra high-speed video camera (40,500 pictures/sec). The heat transfer from shock-compressed high temperature vapor to He II forming a thermal shock wave is considered. The temperature rise ratio of an induced thermal shock to that of an incident gas dynamic shock wave was found to be very small, as small as 0.003 at 1.80K. It is seen that the most part of the heat do not be transmitted into bulk He II because a high density quantized vortex layer is rapidly developed in a thermal boundary layer in the immediate vicinity of the vapor-He II interface. The existence of a thermal boundary layer with a large temperature gradient in which the physical state varies from supercritical helium to He II temperature and the rapid growth up to about 1 mm in thickness of the layer with such as thermal conduction process are measured with the temperature measurements. Besides, it is also found that high compressibility of He II results in formation of a dark zone near the interface region that is extended toward bulk He II.
机译:通过测量具有超导温度传感器的温度变化和具有超高速摄像机的Schlieren可视化方法,研究了通过将气体动态冲击波撞击到Superfluid冲击管设施中的Superfluid冲击管设施中的自由表面的强烈的热冲击波。 40,500张图片/秒)。考虑了从冲击压缩的高温蒸汽转移到HE II的形成热冲击波。发现诱导的热冲击与入射气动态冲击波的温度上升比例非常小,小至1.80k的小于0.003。可以看出,由于高密度量化的涡流层在蒸汽 - HE II接口附近的热边界层中快速地显着,因此热量的大部分的热量不被传递到散装中。具有大温度梯度的热边界层的存在,其中物理状态从超临界氦变化到He II温度,并且通过温度测量与诸如热传导工艺的层厚度高达约1mm的快速生长测量。此外,还发现,HE II的高可压缩性导致在延伸到散装HE II的界面区域附近的暗区的形成。

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