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Direct and Large-Eddy Simulation of Buoyancy-Induced Flows in Rotating Cavities

机译:旋转腔中浮力诱导流动的直接和大涡模拟

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摘要

In this research a spectral element method is used to perform direct numerical simulation (DNS) and implicit large-eddy simulation (LES) of flows induced by centrifugal buoyancy in rotating cavities. These flows occur, for instance, in the compressor cavities of gas turbines internal air systems, in which cooling air is used to extract heat from compressor disks. Buoyancy-induced flows are inherently challenging to study using computational fluid dynamics (CFD), since turbulence models based on the Reynolds-averaged Navier-Stokes (RANS) equations are not able to provide an accurate description of the phenomena induced by the interplay between buoyancy and rotation. For this reason, model-free approaches are desirable, since they can provide an accurate description of the flow physics. First, the method is applied to a rotor/stator configuration, in which regions of laminar, transitional and fully turbulent flow coexist, and the results are compared with experimental data from the literature. Subsequently, flow induced by centrifugal buoyancy in a sealed rotating annulus is investigated using linear stability analysis, DNS and LES. It is shown that the onset of convection for a rotating cavity is similar to that for the problem of Rayleigh-Benard convection. Analysing flow statistics for different values of the Rayleigh number, it is shown that the disk boundary layer behaves as a laminar Ekman layer, both in terms of its thickness and of its velocity profiles. This is observed even when instantaneous profiles are considered, despite the unsteadiness of the solution. The results also show that the shroud thermal boundary layer scaling is consistent with that of natural convection under gravity. Introducing an axial throughflow of cooling air, some features observed in the sealed cavity are maintained, however a strong reduction in the core temperature and a corresponding increase in the shroud heat transfer occur. The axial throughflow also promotes a significant increase in the range of frequencies observed inside the cavity.
机译:在这项研究中,使用频谱元素方法对旋转空腔中的离心浮力引起的流动进行直接数值模拟(DNS)和隐式大涡模拟(LES)。这些流动例如发生在燃气轮机内部空气系统的压缩机腔中,在该压缩机腔中,冷却空气用于从压缩机盘提取热量。由于使用基于雷诺平均Navier-Stokes(RANS)方程的湍流模型无法准确描述由浮力之间的相互作用引起的现象,因此使用计算流体动力学(CFD)研究浮力产生的流动具有固有的挑战性。和旋转。由于这个原因,无模型方法是可取的,因为它们可以提供对流动物理学的准确描述。首先,将该方法应用于转子/定子构造,其中层流,过渡和完全湍流区域共存,并将结果与​​文献中的实验数据进行比较。随后,使用线性稳定性分析,DNS和LES研究了密封旋转环中离心浮力引起的流动。结果表明,旋转腔的对流开始与瑞利-贝纳德对流问题相似。对瑞利数的不同值进行流量统计分析,结果表明,磁盘边界层在厚度和速度分布方面均表现为层状埃克曼层。即使解决方案不稳定,即使考虑瞬时轮廓,也可以观察到这一点。结果还表明,罩的热边界层结垢与重力作用下的自然对流一致。通过引入冷却空气的轴向流,可以保持在密封腔中观察到的某些特征,但是会大大降低堆芯温度,并相应增加护罩的热传递。轴向通流还促进腔体内观察到的频率范围的显着增加。

著录项

  • 作者

    Berta Pitz, Diogo.;

  • 作者单位

    University of Surrey (United Kingdom).;

  • 授予单位 University of Surrey (United Kingdom).;
  • 学科 Mechanical engineering.;Fluid mechanics.
  • 学位 Ph.D.
  • 年度 2018
  • 页码 167 p.
  • 总页数 167
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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