含导弹的内埋弹舱缩比模型空腔噪声试验研究  

Experiment Research on Cavity Noise of Scale Model of Internal Weapon Bay Including Missiles

作　　者：王琰[1] 郭定文[1] 刘兴强[1] 

机构地区：[1]中国飞机强度研究所航空噪声与动强度航空科技重点实验室,西安710065

出　　处：《科学技术与工程》2017年第8期298-302,共5页Science Technology and Engineering

摘　　要：通过试验的方法研究了含弹的内埋弹舱缩比模型的空腔噪声。研究了不同的来流速度、前缘扰流板、后缘挡板等对含弹的内埋弹舱空腔噪声的影响。通过试验得出结论,来流速度影响空腔内的噪声分布,弹舱的纯音频率也会发生变化;带锯齿的前缘扰流板对弹舱内噪声不会起到抑制作用,反而会增大弹舱内噪声;后缘挡板倾斜角度越大,对弹舱内噪声的抑制效果越好。The cavity noise of scale model of internal weapon bay including missiles were studied in the anechoic laboratory. The effect of weapon bay on cavity noise is researched,by different permanents through experiment,such as flow velocity,the leading edge spoiler,angle of the trailing edge. Conclusions could be drew as following：flow velocity can impact the distribution and frequency of the cavity noise. The leading edge of spoiler with saw tooth would not achieve the effect of noise suppression. With the increasing of the angle of the trailing edge,the cavity noise suppression effect is more obvious.

关 键 词：内埋弹舱 空腔噪声 扰流板 后缘挡板倾角 

分 类 号：V211.7[航空宇航科学与技术—航空宇航推进理论与工程]