【24h】

STRUCTURE DETECTION AND ANALYSIS OF NON-CIRCULAR IMPINGING JETS IN A SEMI-CONFINED ARRAY CONFIGURATION

机译:半约束阵列结构中非圆形冲击射束的结构检测与分析

获取原文
获取原文并翻译 | 示例

摘要

The modal kinetic energy distribution and instantaneous vortex field of an impinging confined jet array is investigated. The jet array consists of 7-by-7 equally spaced orifice nozzles, using two nozzle cross sections: circular and cusped ellipse. Digital Particle Image Velocimetry (DPIV) is used to determine the velocity field of the impinging jets along the center row in the plane parallel with the cross flow direction. Proper Orthogonal Decomposition (POD) and vortex detection algorithms are used to analyze the results of 50 instantaneous velocity fields in the impingement regions for each of several jets located along the crossflow direction. The energetic content of the flow is evaluated based on the POD eigenvalue distribution, the number of POD modes necessary to reconstruct the instantaneous velocity field, and the modal turbulent kinetic energy distributions. Vortex detection algorithms are used to locate and quantify the nature of the instantaneous vortices within the flow. Results of the vortex identification and the associated kinetic energy distribution within the flows are used to indicate the overall sensitivity to the nozzle geometry. The results suggest that the cusped ellipse nozzle when oriented with its major axis parallel to the flow, because of axis switching, can provide increased surface interactions which may lead to enhanced rates of heat and mass transfer.
机译:研究了撞击受限射流阵列的模态动能分布和瞬时涡流场。射流阵列由7×7等距孔口喷嘴组成,使用两个喷嘴横截面:圆形和尖头椭圆形。数字粒子图像测速(DPIV)用于确定撞击射流在平行于横流方向的平面中沿着中心行的速度场。适当的正交分解(POD)和涡流检测算法用于分析沿横流方向定位的几条射流在撞击区域中的50个瞬时速度场的结果。根据POD特征值分布,重构瞬时速度场所需的POD模式数量以及模态湍动能分布,评估流的能量含量。涡流检测算法用于定位和量化流中瞬时涡流的性质。涡流识别的结果以及流中相关的动能分布用于指示对喷嘴几何形状的总体敏感性。结果表明,由于轴切换,尖头椭圆形喷嘴的长轴平行于流定向时,可以提供增加的表面相互作用,从而可能导致热量和质量传递速率提高。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号