首页> 外文学位 >Laser manipulation of atomic and molecular flows.
【24h】

Laser manipulation of atomic and molecular flows.

机译:原子和分子流的激光操纵​​。

获取原文
获取原文并翻译 | 示例

摘要

The continuing advance of laser technology enables a range of broadly applicable, laser-based flow manipulation techniques. The characteristics of these laser-based flow manipulations suggest that they may augment, or be superior to, such traditional electro-mechanical methods as ionic flow control, shock tubes, and small scale wind tunnels. In this study, methodology was developed for investigating laser flow manipulation techniques, and testing their feasibility for a number of aerospace, basic physics, and micro technology applications. Theories for laser-atom and laser-molecule interactions have been under development since the advent of laser technology. The theories have yet to be adequately integrated into kinetic flow solvers. Realizing this integration would greatly enhance the scaling of laser-species interactions beyond the realm of ultra-cold atomic physics. This goal was realized in the present study. A representative numerical investigation, of laser-based neutral atomic and molecular flow manipulations, was conducted using near-resonant and non-resonant laser fields. To simulate the laser interactions over a range of laser and flow conditions, the following tools were employed: a custom collisionless gas particle trajectory code and a specifically modified version of the Direct Simulation Monte Carlo statistical kinetic solver known as SMILE. In addition to the numerical investigations, a validating experiment was conducted. The experimental results showed good agreement with the numerical simulations when experimental parameters, such as finite laser line width, were taken into account. Several areas of interest were addressed: laser induced neutral flow steering, collimation, direct flow acceleration, and neutral gas heating. Near-resonant continuous wave laser, and non-resonant pulsed laser, interactions with cesium and nitrogen were simulated. These simulations showed trends and some limitations associated with these interactions, used for flow steering and collimation. The use of one of these interactions, the induced dipole force, was extended beyond a single Gaussian laser field. The interference patterns associated with counter-propagating laser fields, or "optical lattices," were shown to be capable of both direct species acceleration and gas heating. This study resulted in predictions for a continuous, resonant laser-cesium flow with accelerations of 106 m/s2. For this circumstance, a future straightforward proof of principle experiment has been identified. To demonstrate non-resonant gas heating, a series of pulsed optical lattices were simulated interacting with neutral non-polar species. An optimum time between pulses was identified as a function of the collisional relaxation time. Using the optimum time between pulses, molecular nitrogen simulations showed an increase in gas temperature from 300 K to 2470 K at 1 atm, for 50 successive optical lattice pulses. A second proof of principle experiment was identified for future investigation.
机译:激光技术的不断发展使一系列广泛适用的基于激光的流量操纵技术成为可能。这些基于激光的流量操纵的特性表明,它们可以增强或优于诸如离子流量控制,激波管和小型风洞之类的传统机电方法。在这项研究中,开发了用于研究激光流操纵技术并测试其在航空航天,基础物理学和微技术应用中的可行性的方法。自激光技术问世以来,有关激光-原子和激光-分子相互作用的理论一直在发展中。这些理论尚未充分整合到动力学流求解器中。实现这种整合将大大增强超物种原子物理领域之外的激光物种相互作用的规模。本研究实现了这一目标。使用近共振和非共振激光场进行了基于激光的中性原子和分子流操纵的代表性数值研究。为了模拟在一定范围的激光和流动条件下的激光相互作用,使用了以下工具:自定义的无碰撞气体粒子轨迹代码和直接模拟蒙特卡洛统计动力学求解器的特殊修改版本,称为SMILE。除了数值研究外,还进行了验证实验。考虑到有限的激光线宽等实验参数,实验结果与数值模拟吻合良好。解决了几个感兴趣的领域:激光诱导的中性流转向,准直,直流加速和中性气体加热。模拟了近共振连续波激光器和非共振脉冲激光器与铯和氮的相互作用。这些模拟显示了趋势和与这些相互作用相关的一些限制,用于流量控制和准直。这些相互作用之一(感应偶极力)的使用已扩展到单个高斯激光场之外。与反向传播的激光场或“光学晶格”相关的干涉图样显示出能够直接加速物质和加热气体。这项研究得出的预测是,加速度为106 m / s2的连续共振激光铯流。在这种情况下,已经确定了将来进行原理实验的直接证明。为了演示非共振气体加热,模拟了一系列脉冲光学晶格与中性非极性物质的相互作用。脉冲之间的最佳时间被确定为碰撞弛豫时间的函数。使用脉冲之间的最佳时间,分子氮模拟显示,对于50个连续的光学晶格脉冲,气体温度在1个大气压下从300 K增加到2470K。确定了第二项原理验证实验,以供将来研究。

著录项

  • 作者

    Lilly, Taylor C.;

  • 作者单位

    University of Southern California.;

  • 授予单位 University of Southern California.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 133 p.
  • 总页数 133
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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