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Bubble formation and detachment from a wall orifice in a liquid cross flow under low and normal gravity.

机译:在低重力和法向重力下,液体以横流形式从壁孔中形成气泡并从壁孔中脱离。

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摘要

Bubble formation and detachment is an integral part of the two-phase flow science. The objective of the present work is to experimentally and theoretically investigate the effects of liquid cross-flow velocity, gas flow rate, and orifice diameter on bubble formation in a wall-bubble injection configuration. The effects of high and low gas momentum flux regimes on the bubble diameter at detachment are investigated experimentally. Bubble formation and detachment experiments were performed under normal and low gravity using the NASA DC-9 Reduced Gravity Aircraft facility. The experimental results show that bubble formation and detachment depends on gravity, the orifice diameter, the gas flow rate, and the liquid cross-flow velocity. Using scaling and a force balance, two different detachment mechanisms are identified. When the gas momentum is large, the bubble detaches from the injection orifice as the gas momentum overcomes the attaching effects of liquid drag and inertia. The surface tension force is much reduced because a large part of the bubble pinning edge at the orifice is lost as the bubble axis is tilted by the liquid flow. When the gas momentum is small, the force balance in the liquid flow direction is important, and the bubble detaches when the bubble axis inclination exceeds a certain angle.; A theoretical model based on a force balance on the bubble is proposed in this work. Predictions of the model that reasonably agree with the experimental results, suggest that the surface tension that represents a major attaching force, is being compromised by a detaching force responsible for loss of pinning. We propose in this work that this force scales with the orifice radius and acts upward and contributes to bubble detachment. Two detachment criteria were applicable depending on the gas to liquid momentum force ratio. Inclusion of this proposed force in the low gravity models results in good agreement with the experimental trends of the bubble diameter at detachment. Effect of this detaching force on normal gravity model prediction was negligible. Comparison was made with 2-dimensional normal gravity models based on Kumar-Kuloor formulation.
机译:气泡的形成和分离是两相流科学的组成部分。本工作的目的是从实验和理论上研究壁泡喷射配置中液体错流速度,气体流速和孔口直径对气泡形成的影响。实验研究了高和低气体动量通量制度对分离时气泡直径的影响。使用NASA DC-9重力降低飞机装置在正常和低重力下进行了气泡形成和脱离实验。实验结果表明,气泡的形成和脱离取决于重力,孔口直径,气体流速和液体错流速度。使用缩放和力平衡,可以确定两种不同的分离机制。当气体动量较大时,由于气体动量克服了液体阻力和惯性的附着作用,气泡会从喷射孔中脱离。由于当气泡轴线由于液体流倾斜而损失了孔口处的气泡钉扎边缘的大部分时,表面​​张力大大降低了。当气体动量较小时,在液体流动方向上的力平衡很重要,并且当气泡轴线的倾角超过一定角度时,气泡分离。本文提出了一种基于气泡上力平衡的理论模型。该模型的预测与实验结果合理地吻合,表明代表主要附着力的表面张力正在受到造成钉扎损失的分离力的影响。我们在这项工作中建议,该力与孔口半径成比例,并向上作用并有助于气泡脱离。取决于气液动量比,有两个分离标准适用。在低重力模型中包含此提议的力会导致与气泡直径在分离时的实验趋势保持一致。该分离力对正常重力模型预测的影响可忽略不计。使用基于Kumar-Kuloor公式的二维法向重力模型进行了比较。

著录项

  • 作者

    Nahra, Henry K.;

  • 作者单位

    Case Western Reserve University.;

  • 授予单位 Case Western Reserve University.;
  • 学科 Physics Fluid and Plasma.; Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 190 p.
  • 总页数 190
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 等离子体物理学;机械、仪表工业;
  • 关键词

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