减少减速阶段以减轻直接驱动集成电路框架内爆中流体动力不稳定性的负面影响

M. Temporal, A. R. Piriz, B. Canaud, Rafael Ramis
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摘要

在惯性约束聚变舱内爆的减速阶段,雷利-泰勒流体力学不稳定性会影响甚至熄灭点火和热核燃料波的传播。这种不稳定性往往会将内部的热等离子体与冷的致密等离子体外壳混合在一起,形成一个混合层,从而抑制核聚变反应。我们使用一维流体力学代码 Multi-IFE 模拟了直驱高增益激光器-胶囊设计的内爆,并估算了混合层平均半径和厚度的时间演变。为了模拟反应速率降低的效果,混合层中的燃料反应性被人为设置为零,从而抑制了燃烧波在混合层中的传播,使能量增益无效。为了克服这种负面影响,我们建议加入二次短脉冲和强激光脉冲,以缩短减速阶段的持续时间,进而减小混合层的厚度。为了确定能够恢复高能量增益的最佳次级激光脉冲,我们进行了一项研究。
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Reduction of the deceleration phase to mitigate the negative effect of hydrodynamic instabilities in direct-drive ICF implosions
In the deceleration phase of an Inertial Confinement Fusion capsule implosion Rayleigh-Taylor hydrodynamic instability can affect or even quench the ignition and thermonuclear burn wave propagation. This instability tends to mix the inner hot plasma with the cold and dense plasma shell providing a mixing layer where nuclear fusion reactions are inhibited. The 1D hydrodynamic code Multi-IFE has been used to simulate the implosion of a direct-drive high-gain laser-capsule design and the temporal evolution of the average radius and thickness of the mixing layer have been estimated. To mimic the effect of the reduced reaction rate the fuel reactivity in the mixing layer has been artificially set to zero thus inhibiting the burn wave propagation throughout it nullifying the energy gain. In order to overcome this negative effect is proposed the addition of secondary short and powerful laser pulse that would reduce the duration of the deceleration phase, which in turn get smaller the thickness of the mixing layer. A study has been performed to identify the optimal secondary laser pulse that allows recover the high energy gain.
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