用迪安法和直接法测定蜂窝状谐振器的阻抗

IF 0.1 Q4 ACOUSTICS Akustika Pub Date : 2021-01-01 DOI:10.36336/akustika20214125
I. Khramtsov, V. Palchikovskiy, O. Kustov
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引用次数: 0

摘要

本文在对声波掠入射蜂窝谐振腔内物理过程进行数值模拟的基础上,研究了声学衬里试样阻抗的确定问题。计算域为带声衬垫样品的掠入射阻抗管的测试截面。衬里样品为单个蜂窝谐振器,深度为14mm,开放面积为4.2%。基于非平稳可压缩enavier - stokes方程的三维直接解,进行了数值模拟。在数值模拟中记录压力-时间和速度-时间信号,采用迪恩法和直接法(声压与正常声速之比)进行处理。两种方法得到的阻抗比较表明,两者吻合较好。
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DETERMINATION OF THE IMPEDANCE OF A HONEYCOMB RESONATOR BY DEAN’S METHOD AND DIRECT METHOD IN A COMPUTATIONAL EXPERIMENT WITH GRAZING INCIDENCE OF WAVES
The article considers the determination of the impedance of the acoustic liner sample on the basis of numerical simulation of physical processes in a honeycomb resonator with a grazing incidence of sound waves. The computational domain is the test section of a grazing incidence impedance tube with an acoustic liner sample. The liner sample is a single honeycomb resonator with a depth of 14 mm and an open area percent of 4.2%. Numerical simulation is performed based on the direct solution of the non-stationary compressible Navier-Stokes equations in a three-dimensional formulation. The pressure-time and velocity-time signals are recorded in the numerical simulation and processed by Dean's method and the direct method (from the ratio of acoustic pressure to normal acoustic velocity). The comparison of impedances obtained by the two methods demonstrates a good agreement with each other.
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来源期刊
Akustika
Akustika ACOUSTICS-
CiteScore
0.80
自引率
0.00%
发文量
4
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