Numerical computation and improvement of aerodynamic radiation noises of pantographs

This paper studied the aerodynamic characteristics of cylinder and pantograph based on large eddy simulation and the acoustic boundary element method, compared sound pressure levels of different observation points and adopted measures to reduce radiation noises. Pressure distributions on the upper a...

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Main Author: Jin-mei Wu
Format: Article
Language:English
Published: JVE International 2017-08-01
Series:Journal of Vibroengineering
Subjects:
Online Access:https://www.jvejournals.com/article/18300
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spelling doaj-e4ba62878c9d4762a0d2d92fa7c2c2a72020-11-24T20:40:17ZengJVE InternationalJournal of Vibroengineering1392-87162538-84602017-08-011953939395210.21595/jve.2017.1830018300Numerical computation and improvement of aerodynamic radiation noises of pantographsJin-mei Wu0North China University of Water Resources and Electric Power,Zhengzhou, ChinaThis paper studied the aerodynamic characteristics of cylinder and pantograph based on large eddy simulation and the acoustic boundary element method, compared sound pressure levels of different observation points and adopted measures to reduce radiation noises. Pressure distributions on the upper and lower surfaces of the cylinder were symmetrical, and radiation noises were basically the same too. Sound pressure level in the front of the cylinder was more than that on the upper and lower surfaces of the cylinder. Sound pressure level at the back of the cylinder was the maximum. With the increase of the computational time, shedding vortexes gradually developed backwards, and the influence area was bigger. The radius of radiation sound field of the cylinder was obviously reduced after applying porous materials. Additionally, contours for noise were highly symmetrical in the whole analyzed frequency band. At 2000 Hz, the cylinder presented the obvious characteristics of dipole noise source. The aerodynamic drag and lift of pantographs through numerical computation were similar to experimental results and increased with the increase of flow velocity, which showed that the computational model for the aerodynamic characteristics of pantographs in this paper was effective. Pressure was large in the area close to the pantograph head, in the connection position between upper and lower pull rods and near the base. Long dragged airflow was formed at the pantograph head, upper and lower pull rods and at the back of the base, which had a serious influence on the distribution of aerodynamic noises of pantographs. Obvious shedding vortexes were formed in the area far away from the pantograph rather than near the pantograph. The density and strength of shedding vortexes were not large. Sound pressure levels of observation points which had the same distance from the center of pantograph base were basically the same in change trend, value and peak frequency. However, the sound pressure level of observation points around the pantograph head was obviously greater than that of other observation points when the analyzed frequency was over 1000 Hz. Radiation noises in the connection position between upper and lower pull rods were greater than that of other observation points. With the increase of the analyzed frequency, the dispersive-ness of aerodynamic noises of pantographs was increasingly obvious. The radiation noise of pantographs was mainly spread along the inclined plane of 45°. When a layer of porous materials was covered on the surface of pantographs, the influence area of radiation noises was obviously reduced. In addition, the sound pressure level of radiation noises was improved.https://www.jvejournals.com/article/18300flow fieldaerodynamic radiation noisecylinderpantographporous materials
collection DOAJ
language English
format Article
sources DOAJ
author Jin-mei Wu
spellingShingle Jin-mei Wu
Numerical computation and improvement of aerodynamic radiation noises of pantographs
Journal of Vibroengineering
flow field
aerodynamic radiation noise
cylinder
pantograph
porous materials
author_facet Jin-mei Wu
author_sort Jin-mei Wu
title Numerical computation and improvement of aerodynamic radiation noises of pantographs
title_short Numerical computation and improvement of aerodynamic radiation noises of pantographs
title_full Numerical computation and improvement of aerodynamic radiation noises of pantographs
title_fullStr Numerical computation and improvement of aerodynamic radiation noises of pantographs
title_full_unstemmed Numerical computation and improvement of aerodynamic radiation noises of pantographs
title_sort numerical computation and improvement of aerodynamic radiation noises of pantographs
publisher JVE International
series Journal of Vibroengineering
issn 1392-8716
2538-8460
publishDate 2017-08-01
description This paper studied the aerodynamic characteristics of cylinder and pantograph based on large eddy simulation and the acoustic boundary element method, compared sound pressure levels of different observation points and adopted measures to reduce radiation noises. Pressure distributions on the upper and lower surfaces of the cylinder were symmetrical, and radiation noises were basically the same too. Sound pressure level in the front of the cylinder was more than that on the upper and lower surfaces of the cylinder. Sound pressure level at the back of the cylinder was the maximum. With the increase of the computational time, shedding vortexes gradually developed backwards, and the influence area was bigger. The radius of radiation sound field of the cylinder was obviously reduced after applying porous materials. Additionally, contours for noise were highly symmetrical in the whole analyzed frequency band. At 2000 Hz, the cylinder presented the obvious characteristics of dipole noise source. The aerodynamic drag and lift of pantographs through numerical computation were similar to experimental results and increased with the increase of flow velocity, which showed that the computational model for the aerodynamic characteristics of pantographs in this paper was effective. Pressure was large in the area close to the pantograph head, in the connection position between upper and lower pull rods and near the base. Long dragged airflow was formed at the pantograph head, upper and lower pull rods and at the back of the base, which had a serious influence on the distribution of aerodynamic noises of pantographs. Obvious shedding vortexes were formed in the area far away from the pantograph rather than near the pantograph. The density and strength of shedding vortexes were not large. Sound pressure levels of observation points which had the same distance from the center of pantograph base were basically the same in change trend, value and peak frequency. However, the sound pressure level of observation points around the pantograph head was obviously greater than that of other observation points when the analyzed frequency was over 1000 Hz. Radiation noises in the connection position between upper and lower pull rods were greater than that of other observation points. With the increase of the analyzed frequency, the dispersive-ness of aerodynamic noises of pantographs was increasingly obvious. The radiation noise of pantographs was mainly spread along the inclined plane of 45°. When a layer of porous materials was covered on the surface of pantographs, the influence area of radiation noises was obviously reduced. In addition, the sound pressure level of radiation noises was improved.
topic flow field
aerodynamic radiation noise
cylinder
pantograph
porous materials
url https://www.jvejournals.com/article/18300
work_keys_str_mv AT jinmeiwu numericalcomputationandimprovementofaerodynamicradiationnoisesofpantographs
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