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Canada and NATO Operations:Examining the ‘middle power’ narrative and its influence on Canadian foreign policy in NATO’s Afghanistan and Libya operations

机译:加拿大和北约行动:在北约的阿富汗和利比亚行动中研究“中间国家”的叙述及其对加拿大外交政策的影响

摘要

Nickel-based superalloys are high performance structural materials that exhibitexcellent strength and creep resistance at high temperatures, even inchemically aggressive environments. This makes them ideal for use in theconstruction of ecient turbines for energy generation or aerospace applications.These superalloys are usually manufactured as single crystals, withtheir high strength resulting from dislocation pinning at interfaces betweenthe fcc matrix an L12-ordered precipitates. Chemical impurities such asrhenium also aect dislocation mobility, and their inclusion in commercialmaterials is standard practice. However, there is currently no detailed understandingof the atomic-scale mechanisms underlying these processes. Thisproblem is here addressed at the atomistic level. The typical accuracy level ofrst principle methods is required to describe bond breaking in the distortedregion surrounding a dislocation core and for including impurities in the fccmatrix, but model systems must be large enough to accommodate the straingradients typical of long-range elastic interactions due to the presence ofdislocations. Multiscale methods are therefore required for simulating thesechemo-mechanical processes. The `Learn on the Fly' (LOTF) technique is anon-uniform precision quantum mechanical/molecular mechanical approach.It oers a predictor/corrector algorithm for speeding up calculations, and thepossibility of modelling a moving quantum region, useful for fast dislocationmotion due to high simulating temperature or load condition. The scope ofthis thesis is to apply this method to metallic systems to conduct, for the rsttime, quantum mechanical accurate simulations of dislocation motion in Nibasedalloys. The QM/MM method corrects the deciencies of the classicalinteratomic potential related to inaccurate energetics for the hcp phase, relevantto the geometry of dislocation cores, and it is capable of reproducing thecorrect separation between Shockley partials at high temperature conditions.
机译:镍基高温合金是高性能的结构材料,即使在化学侵蚀的环境下,也能在高温下表现出出色的强度和抗蠕变性。这使得它们非常适合用于制造用于能源发电或航空航天的新型涡轮机。这些超级合金通常以单晶形式制造,其高强度是由于错位钉扎在fcc基质之间的界面上,形成了L12级析出物。化学杂质(例如also)也会影响位错迁移率,将它们包含在商业材料中是标准做法。但是,目前尚不了解这些过程背后的原子尺度机理。这个问题在原子层次上得到解决。需要使用第一原理方法的典型精度水平来描述位错核心周围扭曲区域中的键断裂,并在fccmatrix中包含杂质,但是模型系统必须足够大,以适应由于存在而引起的远距离弹性相互作用的典型应变梯度位错。因此,需要采用多尺度方法来模拟这些化学机械过程。 ``飞行中学习''(LOTF)技术是一种非均匀的精确量子力学/分子力学方法,它提供了一种预测器/校正器算法来加快计算速度,并且可以对移动的量子区域进行建模,这对于由于以下原因导致的快速位错运动很有用:高仿真温度或负载条件。本文的范围是将这种方法应用到金属系统中,以便首次对镍基合金中的位错运动进行量子力学的精确模拟。 QM / MM方法校正了与位错核的几何形状有关的,与hcp相的不正确的高能学有关的经典原子间势的衰变,并且能够在高温条件下重现Shockley部分之间的正确间距。

著录项

  • 作者

    Wolfraim Zachary Aidan;

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  • 年度 2016
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  • 原文格式 PDF
  • 正文语种 eng
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