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Liner impedance modification by varying perforate orifice geometry.

机译:通过改变穿孔的孔口几何形状来改变衬管阻抗。

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The present work explored the feasibility of controlling the acoustic impedance of a resonant type acoustic liner. This was accomplished by translating one perforate over another of the same porosity creating a totally new perforate that had an intermediate porosity. This type of adjustable perforate created a variable orifice perforate whose orifices were non-circular. This arrangement also formed a stepped geometry in the transverse direction, referred to here as a stepped oval orifice. The key objective of the present study was to quantify the degree of attenuation control that can be achieved by using such a concept on the buried septum in a two-degree-of-freedom acoustic liner. An additional objective was to examine the adequacy of the existing impedance models to explain the behavior of the unique orifice shapes that result from the proposed sliding perforate concept. Different orifice shapes with the same area were also examined to determine if highly non-circular orifices had a significant impact on the impedance. This was primarily an experimental study consisting of normal incidence impedance measurements and flow-duct insertion and transmission loss measurements. The flow-duct measurements were made with grazing flow velocities up to 76.2 m/s (250 ft/s). It was found that perforate translational movements on the order of the orifice diameter (1.6 mm) resulted in shifting of the primary resonance frequency of the liner approximately 14% (200 Hz) and the secondary frequency approximately 16% (800 Hz). Mass reactance values derived from impedance tube measurements of the variable orifice perforate were found to be lower than dim predicted by available theoretical models. This effect was more pronounced at lower porosities where the orifice shapes were highly non-circular. A single stepped oval orifice was also found to have lower mass reactance, compared to a single circular orifice. This could not be predicted by available theoretical models of elliptical shaped orifices. Flow-visualization of the stepped oval orifice revealed that the typical orifice jetting accompanying sound/orifice interactions was “vectored” or deflected off the orifice centerline. Other highly non-circular orifice shapes tested, such as star-shaped, resulted in higher absorption at lower incident sound pressure levels.
机译:本工作探讨了控制谐振型声波衬管的声阻抗的可行性。这是通过将一个孔眼平移到另一个具有相同孔隙度的孔眼上,从而创建一个具有中等孔隙度的全新孔眼来完成的。这种类型的可调节孔眼产生了可变孔眼,其孔眼是非圆形的。这种布置还在横向上形成阶梯状的几何形状,在此称为阶梯状的椭圆孔。本研究的主要目的是量化在两自由度声波衬管中的埋入式隔垫上使用这种概念可以实现的衰减控制程度。另一个目的是检查现有阻抗模型的充分性,以解释所提出的滑动孔眼概念导致的独特孔口形状的行为。还检查了具有相同面积的不同孔形状,以确定高度非圆形的孔是否对阻抗有重大影响。这主要是一项实验研究,包括法向入射阻抗测量以及流道插入和传输损耗测量。掠流速度高达76.2 m / s(250 ft / s)时进行流道测量。发现孔口直径(1.6mm)量级的穿孔平移运动导致衬套的初级共振频率偏移约14%(200Hz),而次级共振频率偏移约16%(800Hz)。发现从可变孔眼的阻抗管测量得出的质量电抗值低于可用理论模型预测的暗淡值。在孔的形状高度非圆形的较低孔隙率下,这种效果更为明显。与单个圆形孔口相比,还发现单个阶梯形椭圆孔口具有较低的质量电抗。可用椭圆形孔的理论模型无法预测这一点。阶梯形椭圆孔口的流动可视化显示,伴随声音/孔口相互作用的典型孔口喷射是“矢量化的”或偏离孔口中心线。测试的其他高度非圆形的孔形状(例如星形)在较低的入射声压水平下会产生更高的吸收。

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