首页> 外文期刊>Physics of plasmas >Computational study of instability and fill tube mitigation strategies for double shell implosions
【24h】

Computational study of instability and fill tube mitigation strategies for double shell implosions

机译:对双壳体灌注造成不稳性和填充管缓解策略的计算研究

获取原文
获取原文并翻译 | 示例
           

摘要

Double shell capsules are an attractive alternative scheme for achieving robust alpha-heating at the National Ignition Facility due to their low convergence ratio and low predicted temperature for achieving volume ignition. Nevertheless, simulations suggest that double shell targets are more susceptible to the fill tube, used to fill the inner shell with liquid DT, than typical single-shell ignition capsule designs, due to the higher density gradient between the shell and the fill tube hole, a lower outer shell velocity, which prevents the implosion from catching up to the initial fill tube jet, and the absence of a rebounding shock through the foam to slow this jet. Double shells are also highly susceptible to the Rayleigh-Taylor instability at both interfaces with the high density inner shell. Combined, these effects are predicted by radiation-hydrodynamics simulations to reduce fuel confinement and temperature, resulting in reduced performance by a factor of approximate to 20-45, depending on design details, compared to idealized one-dimensional (1D) simulations. We discuss a mitigation strategy for both the interfacial instabilities and the fill tube that is predicted by simulations to decrease the yield degradation to a factor of approximate to 4. The mitigation strategy involves a modification of the capsule geometry as well as the use of a multishock pulse shape. The multishock pulse is required for the fill tube mitigation strategy and has the added benefit of stabilizing perturbations at the foam/pusher interface without decreasing 1D yield. In order to experimentally verify these predictions, we discuss the potential use of a hydrogrowth radiography platform that could be applied to test the proposed mitigation strategies.
机译:双壳胶囊是一种有吸引力的替代方案,用于在国家点火设施实现鲁棒α加热,由于它们的低收敛比和低预测温度来实现体积点火。然而,模拟表明,双壳靶更容易受到填充管的影响,用于填充液体DT的内壳,而不是典型的单壳点火胶囊设计,由于壳体和填充管孔之间的较高密度梯度,较低的外壳速度,这防止了缩小到初始填充管射流的内部,并且通过泡沫缺乏反弹冲击以减缓这种射流。双壳对两个具有高密度内壳的界面上的瑞利泰勒不稳定性也高。结合,这些效果通过辐射 - 流体动力学模拟来预测,以降低燃料限制和温度,导致与理想的一维(1D)模拟相比的设计细节,使性能降低到20-45。我们讨论了界面不稳定性和填充管的缓解策略,这些阻力由模拟预测到将屈服劣化减少到近似4.缓解策略涉及胶囊几何形状的修改以及多次ock的使用脉冲形状。填充管缓解策略需要多频脉冲,并且具有在泡沫/推动器界面处稳定扰动的增加的益处,而不降低1d产量。为了通过实验验证这些预测,我们讨论了可以应用的水流射线照相平台的潜在使用来测试提出的缓解策略。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号