A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow
Consider that the sound dipole source in the flow field is composed of multiple micro-spherical oscillating sources. An aerodynamic sound source identification method is established by the relationship among the oscillating source, the radiated sound pressure, and the pressure gradient of flow in th...
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| Format: | Article |
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MDPI AG
2023-04-01
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| Series: | Mathematics |
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| Online Access: | https://www.mdpi.com/2227-7390/11/9/2070 |
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| author | Hao Zhang Yigang Wang Yupeng Wang |
| author_facet | Hao Zhang Yigang Wang Yupeng Wang |
| author_sort | Hao Zhang |
| collection | DOAJ |
| description | Consider that the sound dipole source in the flow field is composed of multiple micro-spherical oscillating sources. An aerodynamic sound source identification method is established by the relationship among the oscillating source, the radiated sound pressure, and the pressure gradient of flow in the near-wall flow field, and the formula for calculating the sound power of the sound dipole source in unsteady flow is derived. It shows that the power of sound dipole sources is proportional to the square of the oscillating force or pressure gradient. The combination of the formula and CFD method is further applied to the flow around the cylinder, which clearly presents the sound power and location characteristics of sound dipole sources. Further, the relationship between the sound source and the flow separation, or flow vortex shedding, is analyzed. The corresponding correlation analysis is also carried out, which indicates that the sound dipole source exists in a finite area of the attached wall. The front end of the area is at the separation point along the circumferential direction of the wall, and the end is at the location where the separation vortex completely falls off and a trailing vortex begins to form. In addition, the thickness of the area exists along the radial direction and gradually increases backward. |
| first_indexed | 2024-03-11T04:13:36Z |
| format | Article |
| id | doaj.art-d1d44dd8735f4872bbfa710c7e817e89 |
| institution | Directory Open Access Journal |
| issn | 2227-7390 |
| language | English |
| last_indexed | 2024-03-11T04:13:36Z |
| publishDate | 2023-04-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Mathematics |
| spelling | doaj.art-d1d44dd8735f4872bbfa710c7e817e892023-11-17T23:19:36ZengMDPI AGMathematics2227-73902023-04-01119207010.3390/math11092070A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall FlowHao Zhang0Yigang Wang1Yupeng Wang2School of Automotive Studies, Tongji University, Shanghai 201804, ChinaSchool of Automotive Studies, Tongji University, Shanghai 201804, ChinaSchool of Automotive Studies, Tongji University, Shanghai 201804, ChinaConsider that the sound dipole source in the flow field is composed of multiple micro-spherical oscillating sources. An aerodynamic sound source identification method is established by the relationship among the oscillating source, the radiated sound pressure, and the pressure gradient of flow in the near-wall flow field, and the formula for calculating the sound power of the sound dipole source in unsteady flow is derived. It shows that the power of sound dipole sources is proportional to the square of the oscillating force or pressure gradient. The combination of the formula and CFD method is further applied to the flow around the cylinder, which clearly presents the sound power and location characteristics of sound dipole sources. Further, the relationship between the sound source and the flow separation, or flow vortex shedding, is analyzed. The corresponding correlation analysis is also carried out, which indicates that the sound dipole source exists in a finite area of the attached wall. The front end of the area is at the separation point along the circumferential direction of the wall, and the end is at the location where the separation vortex completely falls off and a trailing vortex begins to form. In addition, the thickness of the area exists along the radial direction and gradually increases backward.https://www.mdpi.com/2227-7390/11/9/2070aerodynamic sound dipole sourceflow around circular cylinderComputational Fluid Dynamics (CFD)sound powerturbulence field |
| spellingShingle | Hao Zhang Yigang Wang Yupeng Wang A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow Mathematics aerodynamic sound dipole source flow around circular cylinder Computational Fluid Dynamics (CFD) sound power turbulence field |
| title | A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow |
| title_full | A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow |
| title_fullStr | A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow |
| title_full_unstemmed | A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow |
| title_short | A New Method of Identifying the Aerodynamic Dipole Sound Source in the Near Wall Flow |
| title_sort | new method of identifying the aerodynamic dipole sound source in the near wall flow |
| topic | aerodynamic sound dipole source flow around circular cylinder Computational Fluid Dynamics (CFD) sound power turbulence field |
| url | https://www.mdpi.com/2227-7390/11/9/2070 |
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