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Flow and mixing characteristics of a forward-inclined stack-issued jet in crossflow

机译:在Crossflow中向前倾斜堆叠射流的流量和混合特性

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摘要

The flow and mixing characteristics of a forward-inclined stack-issued jet at various inclination angles (0) and jet-to-crossflow momentum flux ratios (R) were experimentally studied in an open-loop wind tunnel. Flow behaviors were examined using the laser-assisted smoke flow visualization technique. The instantaneous velocities of the upwind-side shear-layer were digitized by a hot-wire anemometer using a high-speed data acquisition system. The instability frequencies in the upwind-side shear-layer vortices were obtained by the fast Fourier transform method. Long-exposure flow images were processed using the binary edge-detection technique to obtain the jet spread width. Transverse dispersion of jet fluids was determined using tracer gas concentration detection. The upwind-side shear-layer vortices revealed four characteristic flow modes: the High impingement-crossflow dominated mode (about θ < 15° and low R), the High impingement-jet flow dominated mode (about 9 < 25° and high R), the Low impingement-crossflow dominated mode (about θ > 15° and low R), and the Low impingement-jet flow dominated mode (about θ > 25° and high R). Increasing 9 in the crossflow dominated regimes eliminated the upwind-side shear-layer vortices, while increasing 9 in the jet flow dominated regimes emphasized the upwind-side shear-layer vortices. Increasing θ at a fixed value of R increased jet spread width in the far field in all modes. In the near field, at x/d < 5 in the High impingement-crossflow dominated regime, the jet spread width was greater than in the Low impingement-crossflow dominated regime. In the jet flow dominated regimes, higher 9 values led to greater jet spread width. Transverse dispersion of the jet fluids approached the jet spread width results. In the Low impingement-jet flow dominated regime, transverse dispersion of the jet fluids was significantly increased compared to the other regimes. In addition, the maximum tracer gas concentration was severely reduced at all axial stages, which implied better dispersion of the jet fluids in this regime.
机译:在一个开环风隧道中实验研究了各种倾斜角(0)和喷射到交叉流动动量通量比(R)的前倾斜堆叠发射射流的流动和混合特性。使用激光辅助烟雾性能可视化技术检查流动性。使用高速数据采集系统,通过热线风速计数字化了挤压侧剪切层的瞬时速度。通过快速的傅里叶变换方法获得挤压侧剪切层涡流中的不稳定频率。使用二进制边缘检测技术处理长曝光流量图像以获得喷射扩散宽度。使用示踪气体浓度检测测定喷射流体的横向分散。上风侧剪切层涡流显示出四种特征流动模式:高冲击 - 横流占主导地面模式(约θ<15°且低r),高冲击喷射流量主导模式(约9 <25°和高r) ,低电平冲击交叉流量主导模式(约θ> 15°且低r),以及低电平冲击喷射流量主导的模式(约θ> 25°和高r)。在跨流导地区的横向剪切层涡流中增加9中的9个,同时喷射流动的侧面剪切制度中的9中增加9,强调了上风侧剪切层涡流。在所有模式下,在R增加的R射流扩散宽度下增加θ。在近场中,在高冲击横流导地位的X / D <5中,喷射宽度大于低冲击横流的主导地位。在喷射流动的主导制度中,较高的9个值导致更大的喷射扩散宽度。喷射流体的横向分散率接近喷射宽度的结果。在低冲击喷射流动的主导区域中,与其他方案相比,喷射流体的横向分散显着增加。此外,在所有轴向阶段严重降低了最大示踪气体浓度,这暗示了在该制度中更好地分散喷射流体。

著录项

  • 来源
    《International Journal of Heat and Fluid Flow》 |2020年第4期|108549.1-108549.13|共13页
  • 作者单位

    Department of Mechanical Engineering National Taiwan University of Science and Technology Taipei 10672 Taiwan Republic of China;

    Department of Mechanical Engineering National Taiwan University of Science and Technology Taipei 10672 Taiwan Republic of China;

    Department of Mechanical Design Engineering National Formosa University Yunlin 63201 Taiwan Republic of China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Jet in crossflow; Jet-fluid dispersion; Shear-layer vortices; Flow structure;

    机译:在交叉流中喷射;喷射流体分散;剪切层涡旋;流动结构;

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