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A Comparative Study of Four Impedance Eduction Methodologies Using Several Test Liners

机译:使用几种测试衬管的四种阻抗传导方法的比较研究

摘要

A comparative study of four commonly used impedance eduction methods is presented for a range of liner structures and test conditions. Two of the methods are restricted to uniform flow while the other two accommodate both uniform and boundary layer flows. Measurements on five liner structures (a rigid-wall insert, a ceramic tubular liner, a wire mesh liner, a low porosity conventional liner, and a high porosity conventional liner) are obtained using the NASA Langley Grazing Flow Impedance Tube. The educed impedance of each liner is presented for forty-two test conditions (three Mach numbers and fourteen frequencies). In addition, the effects of moving the acoustic source from upstream to downstream and the refractive effects of the mean boundary layer on the wire mesh liner are investigated. The primary conclusions of the study are that: (1) more accurate results are obtained for the upstream source, (2) the uniform flow methods produce nearly identical impedance spectra at and below Mach 0.3 but significant scatter in the educed impedance occurs at the higher Mach number, (3) there is better agreement in educed impedance among the methods for the conventional liners than for the rigid-wall insert, ceramic, or wire mesh liner, and (4) the refractive effects of the mean boundary layer on the educed impedance of the wire mesh liner are generally small except at Mach 0.5.
机译:针对一系列衬管结构和测试条件,对四种常用的阻抗减小方法进行了比较研究。其中两种方法仅限于均匀流,而其他两种方法均适用于均匀流和边界层流。使用NASA兰利掠流阻力管获得了五个衬里结构(刚性壁插入物,陶瓷管状衬里,金属丝网衬里,低孔隙率常规衬里和高孔隙率常规衬里)的测量值。给出了在42种测试条件(三个马赫数和十四个频率)下每个衬套的感应阻抗。此外,还研究了声源从上游移动到下游的影响以及平均边界层对丝网衬里的折射影响。该研究的主要结论是:(1)上游源获得了更准确的结果,(2)均匀流动法在0.3马赫或更低的马赫数下产生几乎相同的阻抗谱,但是在较高的马赫里产生的阻抗显着散布马赫数,(3)与常规的内衬,陶瓷或金属丝网衬里相比,常规衬里的方法在感应阻抗方面具有更好的一致性,并且(4)平均边界层对感应衬里的折射作用丝网衬里的阻抗通常很小,只有0.5马赫。

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