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带制退器的膛口射流噪声数值模拟与实验研究

Numerical simulation and experimental study on jet noise from a small caliber rifle with a muzzle brake

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【作者】 赵欣怡周克栋赫雷陆野王佳

【Author】 ZHAO Xinyi;ZHOU Kedong;HE Lei;LU Ye;WANG Jia;School of Mechanical Engineering, Nanjing University of Science and Technology;No.208 Research Institute of China Ordnance Industries;

【通讯作者】 周克栋;

【机构】 南京理工大学机械工程学院中国兵器工业第208研究所

【摘要】 为了研究膛口装置对膛口噪声气动特性的影响,对带膛口制退器的某小口径武器的膛口射流噪声进行了数值模拟和实验研究。采用计算流体力学CFD (computational fluid dynamics)-计算气动声学CAA(computational aeroacoustics)耦合算法对膛口噪声进行数值模拟,即对膛口流场进行瞬态CFD模拟,获取流场数据,然后利用所得到的结果采用声学方程模拟声源信息求解声场。基于数值模拟结果,分析了膛口流场变化及噪声的指向性分布,并与实验结果进行了对比。研究表明:膛口制退器的安装改变了膛口流场结构,影响了膛口射流噪声的指向性分布。计算结果与实验结果的误差小于9%,验证了该计算方法的可行性。研究结果可为膛口射流噪声的预测及膛口制退器的设计提供一定的参考。

【Abstract】 In order to investigate the influence of the muzzle device on the characteristics of muzzle aeroacoustic noise, simulation analysis and experimental research were performed on the jet noise induced by the complex flows discharging from a small caliber rifle with a muzzle brake. A CFD(computational fluid dynamics)-CAA(computational aeroacoustics) hybrid method was applied. The muzzle flow field was calculated by using large eddy simulation and the jet noise was determined by the FW-H(Ffowcs WilliamsHawkings) equation based on the obtained source data. Based on the numerical results, the jet noise directivity was analyzed and the comparison to the experimental results was conducted. Results indicate that the muzzle flow field was changed by the muzzle brake and the directional distribution of the jet noise was also affected. The errors between the calculated and experiment results are less than 9%, therefore the numerical method applied in the paper is feasible. The research result can provide a reference for the prediction of muzzle noise and the design of muzzle brakes.

【基金】 联合基金(6141B02040208)
  • 【文献出处】 爆炸与冲击 ,Explosion and Shock Waves , 编辑部邮箱 ,2019年10期
  • 【分类号】TJ201
  • 【网络出版时间】2019-02-01 09:30
  • 【被引频次】2
  • 【下载频次】185
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