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The development and stability of some non-planar boundary-layer flows.

机译:一些非平面边界层流的发展和稳定性。

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摘要

This thesis presents two problems in the field of fluid mechanics. Both problems concern the flow of a Newtonian viscous fluid in the laminar and early-transitional regimes. Geometrically, they also share the following features: a square corner; a wall boundary layer; and a semi-infinite physical domain.Part 1 of this thesis, comprising Chapters 2–5, considers the laminar flow parallel to a streamwise corner. In Chapter 2 we present an in-depth study of the laminar flow internal to a square corner. The hydrodynamic stability of this flow is the subject of Chapter 3. For the special case of zero pressure gradient, our analysis suggests a critical Reynolds number of Re[subscript]c ≈ 44 000 (based on streamwise distance from the leading edge), indicating that this flow is significantly less stable than the well-known Blasius boundary layer on a semi-infinite flat plate. In Chapter 4 we derive the laminar flow external to a square corner. Finally, in Chapter 5 we summarize our findings and offer some recommendations for future research on laminarand transitional corner flows.Part 2, comprising Chapters 6–10, considers the sudden blockage of steady laminar flow within a circular pipe. Even though the blockage occurs almost instantaneously, the fluid takes an appreciable time to come to rest. Accordingly, Chapter 6 presents a detailed analysis of the laminar-decay process at an arbitrary location upstream of the blockage point. The hydrodynamic stability of this unsteady upstream flow is the subject of Chapters 7 and 8. Chapter 7 uses traditional linear eigenmode theory, originally developed for steady laminar flow, to estimate that the laminar flow is absolutely stable in the event that the pre-blockage Reynolds number does not exceed Re[subscript]c ≈ 450. The linear pseudomode analysis of Chapter 8 yields the substantially lower estimate Re[subscript]c ≈ 115, above which there exists the theoretical possibility of transient growth initiating a ‘bypass’ transition to turbulence. However, after accounting for the transient nature of the underlying flow itself, wehypothesize a significantly higher threshold Re[subscript]c ≈ 1000 for full breakdown of the laminar structure.Chapter 9 rounds off the present work by extending the laminar-flow analysis of Chapter 6 to the immediate vicinity of the blockage point. We present a direct numerical simulation of the complete laminar-decay process within this end-region, highlighting the early-phase development of an unsteady corner boundary layer and the subsequent development of vortices in the interior of the pipe.The thesis concludes in Chapter 10 by summarizing the findings from Part 2 and suggesting some fruitful directions for future research on unsteady pipe flows.
机译:本文提出了流体力学领域的两个问题。这两个问题都涉及层流和早期过渡状态下牛顿粘性流体的流动。从几何上讲,它们还具有以下特征:方角;墙边界层;本文的第1部分,包括第2-5章,考虑了与流向角平行的层流。在第二章中,我们对方形角内部的层流进行了深入研究。该流动的流体力学稳定性是第3章的主题。对于零压力梯度的特殊情况,我们的分析表明,Re [c]≈44 000(基于从前缘到水流的距离)的临界雷诺数,表明这表明该流动的稳定性远低于半无限平板上众所周知的Blasius边界层。在第4章中,我们得出了方形角外部的层流。最后,在第5章中,我们总结了我们的发现,并为以后的laminarand过渡角流研究提供了一些建议。第2部分,第6-10章,考虑了圆形管道内稳定层流的突然阻塞。即使阻塞几乎是瞬间发生的,流体也要花费相当长的时间才能静止。因此,第6章详细分析了阻塞点上游任意位置的层流衰减过程。该不稳定上游流的流体力学稳定性是第7章和第8章的主题。第7章使用传统的线性本征模态理论(最初是为稳定层流开发的)来估计,如果发生预阻塞雷诺,则层流绝对稳定。数量不超过Rec c≈450。第8章的线性伪模态分析得出的估计值Re ec c≈115明显较低,在此之上有理论上的瞬时增长可能会引发从“旁路”过渡到湍流。但是,在考虑了基础流动本身的瞬态性质之后,我们假设层状结构完全破裂的阈值Re [c]≈1000明显更高。第9章通过扩展本章的层流分析来完善当前的工作。 6到堵塞点的附近。我们对端部区域内完整的层流衰减过程进行了直接数值模拟,重点介绍了不稳定角边界层的早期发展以及管道内部涡流的后续发展。论文总结于第10章。通过总结第2部分中的发现,并为未来关于不稳定管道流动的研究提出一些有益的指导。

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    Jewell, Nathaniel David;

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  • 年度 2009
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