NUMERICAL SIMULATION OF THE LIGHT AIRCRAFT PROPELLER NOISE UNDER STATIC CONDITION

IF 0.1 Q4 ACOUSTICS Akustika Pub Date : 2021-01-01 DOI:10.36336/akustika202141100
S. Timushev, A. Yakovlev, P. Moshkov
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引用次数: 5

Abstract

The problem of simulation the noise generated during the operation of the propeller is considered. Calculation methods are described and numerical simulation of the noise of a light aircraft propeller by the acoustic-vortex method is performed. The results of numerical modeling of the tonal components of the propeller noise when operating under static conditions are compared with experimental data and calculation results based on a semiempirical model.
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轻型飞机螺旋桨静态噪声的数值模拟
考虑了螺旋桨运行过程中噪声的仿真问题。介绍了轻型飞机螺旋桨噪声的计算方法,并用声涡法对其进行了数值模拟。对静态工况下螺旋桨噪声音质分量的数值模拟结果与实验数据和基于半经验模型的计算结果进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Akustika
Akustika ACOUSTICS-
CiteScore
0.80
自引率
0.00%
发文量
4
期刊最新文献
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