激光驱动激波管概念的GARPUN krf激光靶实验与数值模拟

V. Zvorykin, V. G. Bakaev, A. Iskakov, I. Lebo, G. Sychugov, V. Tishkin
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引用次数: 3

摘要

我们提出了激光驱动激波管(LST)的概念,用于在气体中产生高超声速激波(SW)和在液体中产生压缩波。这种新的实验室技术可以应用于各种基本的水动力学现象的研究,如激波加速下不同液体和气体接触界面的水动力学不稳定性的发展,物体周围的高超声速气体流动,几微秒时间尺度和十毫米空间尺度上强激波折射和积累的影响。这些问题在惯性约束聚变、宇宙学、天体物理学和航空航天工程中具有重要意义。本文给出了数值模拟和初步实验结果,验证了激光驱动激波管用于研究空气中强SW产生的概念。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
GARPUN KrF-laser-target experiments and numerical simulations on the concept of laser-driven shock tube
We have suggested a concept of laser-driven shock tube (LST) for generation of hypersonic shock waves (SW) in gases and compression waves in liquids. This novel laboratory technique might be applied to the studies of various fundamental hydrodynamic phenomena such as development of hydrodynamic instabilities at contact interfaces between different liquids and gases accelerated by shock waves, hypersonic gas flow around bodies, effects of strong shock wave refraction and cumulation in time scale of several microseconds and space scale of ten millimeters. These problems are of great importance in Inertial Confinement Fusion, comsology, astrophysics, and aerospace engineering. In this paper we present both numerical simulations and first experimental results to verify the laser-driven shock tube concept for studying of strong SW generation in the air.
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