首页> 外文学位 >Coherent structure in a turbulent axisymmetric jet via a vector implementation of the proper orthogonal decomposition.
【24h】

Coherent structure in a turbulent axisymmetric jet via a vector implementation of the proper orthogonal decomposition.

机译:通过适当正交分解的矢量实现,湍流轴对称射流中的相干结构。

获取原文
获取原文并翻译 | 示例

摘要

The coherent structure in the near-field of an axisymmetric turbulent jet at a Reynolds number of 3.8 x 105 and Mach number of 0.3 is experimentally characterized by a vector implementation of the proper orthogonal decomposition (POD). The POD eigenfunctions and associated eigenvalues are extracted at several selected streamwise locations in the initial region. The focus on the near-field is motivated by its importance in numerous technical applications. Results show a rapid energy convergence with POD mode number. Examination of the relative energy contained in the combined azimuthal and radial components of the POD modes reveals that it is comparable to that in the streamwise component. The streamwise evolution of the eigenvalue spectra is characterized by a remarkable variation in the azimuthal mode number energy distribution leading to the dominance of azimuthal mode m = 1 beyond the end of the jet core. In contrast, a scalar implementation using only the streamwise component shows the dominance of mode m = 2 which is consistent with previous scalar implementations of the POD. For a given azimuthal mode number, the eigenvalue spectra exhibit a broad spectral peak which occurs at a constant value of Strouhal number based on local shear layer momentum thickness and jet velocity. The phase information required for a local reconstruction of the jet structure is obtained by projecting the POD eigenmodes onto instantaneous realizations of the flow at fixed streamwise locations. The instantaneous realizations are obtained by utilizing cross-stream arrays of multi-sensor probes in conjunction with linear stochastic estimation (LSE). Results clearly show the local dynamic behavior of each component of the jet structure.
机译:雷诺数为3.8 x 105,马赫数为0.3的轴对称湍流射流近场中的相干结构在实验上通过适当的正交分解(POD)的矢量实现来表征。在初始区域中的几个选定的流向位置提取POD特征函数和关联的特征值。其在众多技术应用中的重要性激发了人们对近场的关注。结果表明,能量随POD模式数快速收敛。对POD模式的组合方位角和径向分量中包含的相对能量进行检查后发现,该能量与流向分量中的相对能量相当。特征值频谱的沿流演化的特征在于,方位模数能量分布的显着变化导致超过射流芯端的方位模m = 1的优势。相反,仅使用流式分量的标量实现显示模式m = 2的优势,这与POD的先前标量实现一致。对于给定的方位模数,本征值谱显示宽谱峰,该谱峰基于局部剪切层动量厚度和射流速度在恒定的Strouhal数处出现。通过将POD本征模式投影到固定流向位置的流的瞬时实现上,可以获得喷射结构局部重建所需的相位信息。通过将多传感器探针的交叉流阵列与线性随机估计(LSE)结合使用,可以获得瞬时实现。结果清楚地表明了射流结构各部分的局部动力学行为。

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