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Large-Eddy Simulations of Accelerating Boundary Layer Flows Over Rough Surfaces.

机译:加速粗糙表面上边界层流动的大涡模拟。

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摘要

Large-eddy simulations are carried out to study the combined effects of roughness and favourable pressure gradient in boundary layer flows, where the high acceleration (on smooth walls) may cause flow reversion to the quasi-laminar state. A sand-grain roughness model is used, with the no-slip boundary condition modeled by an immersed boundary method. The properties and accuracies of the scheme are studied, the roughness model is validated, and the spatial-resolution requirements are determined.;The roughness model is applied to boundary layers subject to mild or strong acceleration, with simulations carried out underlining the effects of three parameters: the acceleration parameter, the roughness height, and the inlet Reynolds number. The roughness effects are limited to the roughness sublayer; the outer layer is affected indirectly only, through the changes that roughness causes in the relaminarization and retransition processes. The roughness significantly affects the inner-layer quantities like the friction velocity and the friction coefficient, while the local Reynolds number, the outer-layer mean velocity, as well as the Reynolds stresses beyond the roughness sublayer, are not sensitive to the roughness. The acceleration decreases the Reynolds stresses in the overlap region and promotes a laminar-like velocity profile. The acceleration leads to stabilization of near-wall structures and causes one-dimensional turbulence. The roughness generates small-scale structures at the bottom wall, which disturb the larger structures originally stabilized by the pressure gradient, leading to a decrease in the Reynolds-stress anisotropy. Roughness increases the Reynolds stresses in the roughness sublayer and tends to restore the fully turbulence flow early. The inlet Reynolds number affects the flow stability by determining the viscous length scale compared to the roughness length scales, and by determining how far the roughness effect extents into the boundary layer.
机译:进行了大涡模拟,以研究边界层流中粗糙度和有利压力梯度的综合影响,其中高加速度(在光滑壁上)可能导致流返回准层状。使用沙粒粗糙度模型,通过沉浸边界方法对防滑边界条件进行建模。研究了该方案的性质和准确性,验证了粗糙度模型,确定了空间分辨率的要求。将粗糙度模型应用于受轻度或强加速度影响的边界层,并通过仿真强调了三种方法的效果。参数:加速度参数,粗糙度高度和入口雷诺数。粗糙度影响仅限于粗糙度子层。外层仅通过粗糙度在再分层化和再转变过程中引起的变化而受到间接影响。粗糙度显着影响内层的数量,例如摩擦速度和摩擦系数,而局部雷诺数,外层平均速度以及超出粗糙度子层的雷诺应力对粗糙度不敏感。加速度减小了重叠区域中的雷诺应力,并促进了层状速度分布。加速度导致近壁结构的稳定并引起一维湍流。粗糙度在底壁处生成小规模的结构,从而干扰了最初由压力梯度稳定的较大结构,从而导致了雷诺应力各向异性的减小。粗糙度增加了粗糙度子层中的雷诺应力,并倾向于尽早恢复完全的湍流。入口雷诺数会通过确定粘性长度刻度(与粗糙度长度刻度)相比较,并确定粗糙度影响延伸到边界层的程度,从而影响流动稳定性。

著录项

  • 作者

    Yuan, Junlin.;

  • 作者单位

    Queen's University (Canada).;

  • 授予单位 Queen's University (Canada).;
  • 学科 Engineering Mechanical.
  • 学位 M.A.Sc.
  • 年度 2011
  • 页码 121 p.
  • 总页数 121
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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