基于数值模拟的双层蜂窝衬垫声学特性测定

IF 0.1 Q4 ACOUSTICS
Akustika Pub Date : 2019-11-01 DOI:10.36336/akustika20193430
I. Khramtsov, O. Kustov, V. Palchikovskiy, R. Bulbovich
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引用次数: 1

摘要

首次通过对正入射干涉仪中物理过程的数值模拟,确定了全尺寸双层声衬样品的声学特性。双层衬垫样品由14个蜂窝单元和70个穿孔组成。蜂窝单元和穿孔的尺寸对应于飞机发动机管道中使用的声学衬垫。基于三维非定常Navier-Stokes方程的解进行了数值模拟。数值模拟得到的声学特性与实验结果高度一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
DETERMINATION OF ACOUSTIC CHARACTERISTICS OF THE DOUBLE-LAYER HONEYCOMB LINER BASED ON NUMERICAL SIMULATION
For the first time, the acoustic characteristics of a full-scale double-layer sample of acoustic liner were determined by numerical simulation of physical processes in an normal incident interferometer. The double-layer liner sample consisted of 14 honeycomb cells and 70 perforation holes. The dimensions of the honeycomb cells and perforation holes correspond to the acoustic liners used in the ducts of aircraft engines. Numerical simulation was carried out based on solution of the unsteady Navier-Stokes equations in three-dimensional formulation. A high degree of agreement of the acoustic characteristics obtained by numerical simulation with experiment was noted.
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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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