|国家科技期刊平台
首页|期刊导航|机械科学与技术|分形及规则布置方柱绕流场及气动噪声特性数值研究

分形及规则布置方柱绕流场及气动噪声特性数值研究OA北大核心CSTPCD

Numerical Simulation of Turbulent Flows and Induced Aerodynamic Noise Around Side-by-side Square Cylinders with Multiscale and Regular Arrangements

中文摘要英文摘要

采用大涡模拟并结合K-FWH声比拟方法对两种具有相同阻塞率的方柱布置(规则布置和分形布置)流场进行数值模拟研究.首先利用前人的单方柱绕流实验和数值结果对本文所使用的大涡模拟方法进行验证,结果表明本文所采用的数值方法能较好的预测绕流问题的湍流特性.研究发现在雷诺数为 104,两类布置方柱尾流场平均阻力系数大致相等.规则布置方柱尾流场旋涡脱落呈现明显的"相位锁定"现象,而分形布置方柱尾流场旋涡脱落杂乱无序.与此同时,声学仿真结果表明两类流场的远场声压级指向分布大致相同.规则布置方柱流场中的噪声呈现"相位锁定"现象,分形布置方柱流场能够改变噪声频谱特性,使低频噪声向高频噪声转移.

In this study,large eddy simulations with the usage of the K-FWH equation are performed to numerically simulate turbulent flows behind two different kind of cylinder arrays(regular and multiscale)with the same blocking ratio.The large eddy simulation methods used in this paper are verified by the previous single-cylinder flow experiments and numerical results.The results show that the numerical method used in this paper can better predict the turbulent characteristics of the flow around the cylinder.Numerical results show that at the Reynolds number of 104,the mean drag coefficient of square cylinders with regular arrangement is approximately equal to that of the square cylinders with multiscale arrangement.Vortex shedding behavior in the case of regular arrangement present an obvious phenomenon of"phase locking",while the vortex shedding in the case of multiscale arrangement is rather chaotic.The far-field distributions of the sound pressure level of the two flow fields are approximately the same.The induced noises in case with the regular array also exhibit similar"phase locking"behavior.In contrast,multiscale arrangement can modify the distribution the noise spectrum and transfer the power from the low-frequency region to the high-frequency region.

陈武;韩斐;周毅

中国空气动力研究与发展中心气动噪声控制重点实验室,四川绵阳 621000||南京理工大学能源与动力工程学院,南京 210094

能源与动力

分形布置大涡模拟声比拟湍流特性气动噪声

multiscale arrangementlarge eddy simulationacoustic analogyturbulence characteristicsaerodynamic noise

《机械科学与技术》 2024 (003)

380-393 / 14

气动噪声控制重点实验室研究基金项目(ANCL20200104)

10.13433/j.cnki.1003-8728.20220268

评论