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Characteristics of a transient diesel fuel spray.

机译:瞬态柴油喷雾的特性。

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摘要

The transient characteristics of a diesel fuel spray have been investigated with the simultaneous measurement of droplet sizes and velocities, and photographic images of the spray.; Measurement of droplet sizes and velocities have been performed at axial positions from the near nozzle (x/d = 41.7) to the far-field (x/d = 250) for a single hole nozzle (d = 0.24) mm). At each position, measurements at several radial positions were obtained. For all measurement locations, operating conditions included four gas-to-liquid density ratios, that cover the range from free atmospheric jets to conditions typical of diesel engines. Photographic images of the spray were taken for the entire spray and local portions of the spray with magnified photographs from two different nozzle holes (d = 0.24 mm and 0.41 mm) at ambient gas pressures ranging from near-vacuum to 1.34 MPa.; Increases in {dollar}rhosb{lcub}rm g{rcub}{dollar}/{dollar}rhosb{lcub}l{rcub}{dollar} resulted in greatly decelerated and extended fuel sprays. Near the nozzle, droplet sizes ranged from the lower limit of the measurement system (2{dollar}mu{dollar}m) to the order of nozzle diameter for all {dollar}rhosb{lcub}rm g{rcub}{dollar}/{dollar}rhosb{lcub}l{rcub}{dollar}. Along the spray axis, the droplet sizes slowly decrease with axial position. At the edge of spray, droplet velocities have shown wave-like behavior. Negative velocity components at the downstream edge at high {dollar}rhosb{lcub}rm g{rcub}{dollar}/{dollar}rhosb{lcub}l{rcub}{dollar} are observed because of vortices formed in the mixing layer.; Photographs showed surface waves at lower {dollar}rhosb{lcub}rm g{rcub}{dollar}/{dollar}rhosb{lcub}l{rcub}{dollar}. The near-nozzle spray angle was largest in the initial stage of the injection and decreased to a relatively constant value after 0.5 msec.; Detailed measurements of drop size and velocity were compared to established stability criteria for different droplet breakup mechanisms, specifically criteria for bag breakup and boundary layer stripping. Comparison with the stability criteria indicates that a majority of droplets in the spray are susceptible to both breakup mechanisms near the injector tip. However, downstream or on the edge of the spray, the spray appears to stabilize and any redistribution of droplet size must apparently be a result of collisions.; Experimentally-determined droplet size and velocity PDF's show characteristics that are strongly dependent on time and spatial position in the spray. Comparisons with computed PDF's show best agreement with the data for the multiparameter-dependent distributions, such as the chi-square or log-hyperbolic distributions.
机译:柴油燃料喷雾的瞬态特性已经通过同时测量液滴的大小和速度以及喷雾的照相图像进行了研究。对于单孔喷嘴(d = 0.24)mm,已经在从近喷嘴(x / d = 41.7)到远场(x / d = 250)的轴向位置进行了液滴尺寸和速度的测量。在每个位置,都获得了几个径向位置的测量值。对于所有测量位置,操作条件包括四种气液密度比,涵盖从自由大气压喷射到柴油机典型条件的范围。在从近真空到1.34MPa的环境气压下,从两个不同的喷嘴孔(d = 0.24mm和0.41mm)上用放大的照片拍摄了整个喷雾和喷雾局部的喷雾图像。 {rhosb {lcub} rm g {rcub} {dollar} / {dollar} rhosb {lcub} l {rcub} {dollar}的增加导致燃油喷雾大大减速和延长。在喷嘴附近,对于所有{rhosb {lcub} rm g {rcub} {dollar} /而言,液滴尺寸范围从测量系统的下限(2 {dollar} mu {dollar} m)到喷嘴直径的数量级/ {dollar} rhosb {lcub} l {rcub} {dollar}。沿着喷雾轴线,液滴尺寸随着轴向位置而逐渐减小。在喷雾的边缘,液滴的速度表现出波状行为。由于在混合层中形成了涡旋,因此在高边缘处观察到下游边缘处的负速度分量。 ;照片显示较低的{rhosb {lcub} rm g {rcub} {dollar} / {dollar} rhosb {lcub} l {rcub} {dollar}处的表面波。近喷嘴喷雾角在注射初期最大,在0.5毫秒后减小到相对恒定的值。将液滴大小和速度的详细测量结果与针对不同液滴破裂机制的既定稳定性标准进行比较,特别是针对袋子破裂和边界层剥离的标准。与稳定性标准的比较表明,喷雾中的大多数液滴都易受喷射器尖端附近的两种分解机制影响。然而,在喷雾的下游或边缘,喷雾似乎稳定了,液滴大小的任何重新分配显然必须是碰撞的结果。实验确定的液滴尺寸和速度PDF所显示的特性在很大程度上取决于喷雾中的时间和空间位置。与计算的PDF的比较显示与多参数相关分布的数据(例如卡方或对数双曲线分布)的最佳一致性。

著录项

  • 作者

    Koo, Ja-Ye.;

  • 作者单位

    The University of Wisconsin - Madison.;

  • 授予单位 The University of Wisconsin - Madison.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1991
  • 页码 347 p.
  • 总页数 347
  • 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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