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Void fraction and bubble size distribution measurements underneath laboratory breaking waves.

机译:实验室破碎波下的空隙率和气泡尺寸分布测量。

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摘要

This thesis describes a series of laboratory experiments that were conducted to study the air entrainment produced underneath mechanical generated deep-water breaking waves.;Two fiber-optic probes were calibrated for making void fraction and bubble size measurements underneath breaking waves. Tests showed that the normalized RMS error in the void fraction measurements was ∼10%. It was also determined that if a minimum of ∼15 individual bubble velocities were averaged, the mean bubble velocities were accurate to +/-10%. The bubble size distribution measured with the probes was compared to the size distribution measured from digital video recordings, and it was found that these two distributions agreed closely with each other.;Three significant events were identified during the breaking process of a plunging wave: the plunging water jet impacting the forward face of the wave; the air cavity collapsing and evolving into a dense bubble cloud: and the splash-up impacting the water surface. Numerical models must be able to accurately predict the timing and nature of these events. There were 13 measurement positions along the plunging wave and the peak void fractions measured inside the bubble cloud varied from 0.024 to 0.97; and the mean void fractions varied from 0.012 to 0.37. For the spilling wave case, there were 4 measurement positions and the mean void fractions at these positions varied from 0.17 to 0.29. Based on ensemble averaged time series of alpha> it was deduced that, for the spilling wave case, the void fraction contours run parallel to the free surface. The speed of advance of the air cavity and the splash-up cloud beneath the plunging wave were estimated to be ∼75 and ∼90% of the phase speed, respectively. For the spilling wave, the speed of advance of the bubble cloud was estimated to be ∼100% of the phase speed.
机译:本文描述了一系列的实验室实验,以研究在机械产生的深水破碎波下产生的空气夹带。校准了两个光纤探头,用于测量破碎波下的空隙率和气泡尺寸。测试表明,空隙率测量中的归一化RMS误差约为10%。还可以确定,如果平均至少约15个独立气泡速度,则平均气泡速度将精确到+/- 10%。将用探头测得的气泡尺寸分布与通过数字视频记录测得的气泡尺寸分布进行比较,发现这两个分布彼此吻合得很好。在冲击波的破裂过程中发现了三个重要事件:急速的喷水冲击波的前脸;空气腔坍塌并演变成浓密的气泡云:飞溅物撞击水面。数值模型必须能够准确预测这些事件的时间和性质。沿冲波有13个测量位置,在气泡云内部测得的峰值空隙率在0.024至0.97之间变化。平均空隙率在0.012至0.37之间。对于溢出波情况,有4个测量位置,这些位置的平均空隙率在0.17至0.29之间变化。根据α的总体平均时间序列,可以推论出,对于溢流波情况,空隙分数轮廓线平行于自由表面。气穴和冲入波下面的飞溅云的前进速度估计分别为相速度的〜75%和〜90%。对于溢流波,气泡云的前进速度估计为相速度的〜100%。

著录项

  • 作者

    Rojas Orozco, German.;

  • 作者单位

    University of Alberta (Canada).;

  • 授予单位 University of Alberta (Canada).;
  • 学科 Engineering Marine and Ocean.;Engineering Environmental.
  • 学位 Ph.D.
  • 年度 2008
  • 页码 215 p.
  • 总页数 215
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 海洋工程;环境污染及其防治;
  • 关键词

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