首页> 外文期刊>International Journal of Aeroacoustics >Sound propagation in a lined nozzle with shear and bias flows
【24h】

Sound propagation in a lined nozzle with shear and bias flows

机译:具有剪切和偏置流动的衬里喷嘴中的声音传播

获取原文
获取原文并翻译 | 示例
           

摘要

In this study, the propagation of waves in a two-dimensional parallel-sided nozzle is considered allowing for the combination of: (a) distinct impedances of the upper and lower walls; (b) upper and lower boundary layers with different thicknesses with linear shear velocity profiles matched to a uniform core flow; and (c) a uniform cross-flow as a bias flow out of one and into the other porous acoustic liner. The model involves an "acoustic triple deck" consisting of third-order non-sinusoidal non-plane acoustic-shear waves in the upper and lower boundary layers coupled to convected plane sinusoidal acoustic waves in the uniform core flow. The acoustic modes are determined from a dispersion relation corresponding to the vanishing of an 8 x 8 matrix determinant, and the waveforms are combinations of two acoustic and two sets of three acoustic-shear waves. The eigenvalues are calculated and the waveforms are plotted for a wide range of values of the four parameters of the problem, namely: (i/ii) the core and bias flow Mach numbers; (iii) the impedances at the two walls; and (iv) the thicknesses of the two boundary layers relative to each other and the core flow. It is shown that all three main physical phenomena considered in this model can have a significant effect on the wave field: (c) a bias or cross-flow even with small Mach number M-0 similar to 0.03 - 0.06 relative to the mean flow Mach number M-infinity similar to 0.3 - 1.2 can modify the waveforms; (b) the possibly dissimilar impedances of the lined walls can absorb (or amplify) waves more or less depending on the reactance and inductance; (a) the exchange of the wave energy with the shear flow is also important, since for the same stream velocity, a thin boundary layer has higher vorticity, and lower vorticity corresponds to a thicker boundary layer. The combination of all these three effects (a-c) leads to a large set of different waveforms in the duct that are plotted for a wide range of the parameters (i-iv) of the problem.
机译:在该研究中,认为在二维平行侧喷嘴中的波在允许:(a)上壁的不同阻抗的组合; (b)上层和下边界层,具有不同厚度的线性剪切速度曲线与均匀的芯流量匹配; (c)均匀的交叉流量作为偏置流出一个并进入另一个多孔声学衬里。该模型涉及由上边界层中的三阶非正弦非平面声学 - 剪切波组成的“声学三层”,耦合到均匀芯流动的对流平面正弦声波。声学模式由对应于8×8矩阵确定剂的消失的分散关系确定,并且波形是两个声学和两组的三个声学剪切波的组合。计算特征值,并将波形绘制出问题的四个参数的宽范围值,即:(I / II)核心和偏置流马赫数; (iii)两个墙壁的阻抗; (iv)相对于彼此相对于彼此和芯流的厚度。结果表明,在该模型中考虑的所有三个主要物理现象都可以对波场具有显着影响:(c)即使具有与平均流量相对于平均流量的小马赫数M-0的偏置或交叉流量即使是0.03-0.06 Mach Number M-Infinity类似于0.3 - 1.2可以修改波形; (b)衬里壁的可能不同的阻抗可以根据电抗和电感或多或少地吸收(或扩增)波浪; (a)利用剪切流的波能的交换也很重要,因为对于相同的流速,薄边界层具有更高的涡度,并且较低的涡度对应于较厚的边界层。所有这三种效果(A-C)的组合导致导管中的大量不同波形,该导管绘制了该问题的广泛参数(I-IV)。

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