Aerodynamic Sound Source Identification Method Based on Flow Around Cylinder
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1.Shanghai Automotive Wind Tunnel Center, Tongji University, Shanghai 201804, China;2.Shanghai Key Laboratory of Vehicle Aerodynamics and Vehicle Thermal Management Systems, Shanghai 201804, China

Clc Number:

U461.1

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    Abstract:

    Taking the aerodynamic sound source generated by the airflow flowing through the solid surface as the research object, based on the acoustic wave equation’s solution of dipole sound source corresponding to the force point source, according to both the relationship between the pressure of the sound source and the pulsation force and the relationship between the pulsation force and the pressure gradient in the flow field, the relationship between the pressure of the dipole sound source and the pressure gradient in the flow field was established. Based on the concept that two dipole sound sources can form a quadrupole sound source, the relationship between the pressure of quadrupole sound source and the pulsation velocity of flow field was also established. Finally, taking the flow around cylinder as the research object, the strength and distribution of the dipole and quadrupole sound sources of the flow around cylinder were obtained with a combination of the above two equations and the numerical simulation method. It is shown that the pressure of the dipole sound source to the far field is determined by ??p?t, and the pressure of the quadrupole sound source to the far field is determined by ?2ur2?t2.

    Reference
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    [10] 张强. 气动声学基础[M].北京:国防工业出版社, 2012.
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WANG Yigang, ZHU Langxian, JIAO Yan, ZHANG Hao. Aerodynamic Sound Source Identification Method Based on Flow Around Cylinder[J].同济大学学报(自然科学版),2022,50(10):1500~1507

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History
  • Received:July 12,2021
  • Online: November 03,2022
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