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The influence of surface perturbations and laminar separation bubble on boundary layer instability by direct numerical solution of the Navier-Stokes equations.

机译:通过Navier-Stokes方程的直接数值解,表面扰动和层流分离气泡对边界层不稳定性的影响。

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摘要

The purpose of this study is to shed more light on the role of surface perturbations and the laminar separation bubble associated with them on the boundary-layer instability and to explore this important flow problem in fluid dynamics further. To accomplish this, the stability characteristics of the separated flow over a flat plate are studied first by means of finite-difference solutions to the unsteady Navier-Stokes (N-S) equations in two-dimensions in stream-function vorticity form using a direct matrix solver. The laminar separation bubble is generated by imposing a decelerated velocity profile at the farfield boundary of the integration domain. The resulting flow field is perturbed by introducing small-amplitude Tollmien-Schlichting (T-S) waves of various frequencies upstream of the bubble. The time-accurate analysis shows that the bubble acts as a strong amplifier of these flow disturbances. A highly nonlinear flow field is shown to develop downstream of the bubble, and strong vortex shedding are shown to occur. Consequently, the results of the direct numerical simulation differ noticeably from those of classic linear stability theory, Orr-Sommerfeld (O-S) solutions, proving that the nonparallel effects, together with the nonlinear interactions, are crucial in this flow problem.; Next, the stability characteristics of the separated flow over a hump are studied by solving the unsteady N-S equations in generalized coordinates numerically. A strong nonlinear interaction between the T-S wave and the separation bubble, formed on the lee-side of the hump, is shown to occur, and it results in periodic shedding of blobs of vorticity from the bubble. This nonlinear interaction, together with the nonparallel flow effects, leads to discrepancies between the growth of the T-S waves predicted by linear (parallel) stability theory and the growth observed in the present simulation.
机译:这项研究的目的是进一步阐明表面扰动和与其相关的层流分离气泡对边界层不稳定性的作用,并进一步探讨流体动力学中的这一重要流动问题。为此,首先使用直接矩阵求解器,通过二维流函数涡度形式的二维非定常Navier-Stokes(NS)方程的有限差分解,研究平板上分离流动的稳定性。 。层流分离气泡是通过在积分域的远场边界处施加减速后的速度分布而生成的。通过在气泡上游引入各种频率的小幅度Tollmien-Schlichting(T-S)波来扰动所得的流场。时间精确的分析表明,气泡是这些流动扰动的强大放大器。气泡的下游显示出高度非线性的流场,并显示出强烈的涡旋脱落。因此,直接数值模拟的结果与经典的线性稳定性理论Orr-Sommerfeld(O-S)解决方案明显不同,证明了非平行效应以及非线性相互作用对于该流动问题至关重要。接下来,通过数值求解广义坐标下的非定常N-S方程,研究了驼峰上分离流的稳定性特征。 T-S波与形成在驼峰背风侧的分离气泡之间发生了强烈的非线性相互作用,这导致气泡周期性地散发涡流斑点。这种非线性相互作用以及非平行流动效应导致线性(平行)稳定性理论预测的T-S波的增长与当前模拟中观察到的增长之间存在差异。

著录项

  • 作者

    Elli, Shahram.;

  • 作者单位

    University of California, Davis.;

  • 授予单位 University of California, Davis.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1992
  • 页码 62 p.
  • 总页数 62
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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