空中受油装置降噪研究  

Reduction of Cabin Noise Induced by Flow Around Air Refueling Pipe

作　　者：罗乖林[1] 王宇[1] 王晋军[1] 

机构地区：[1]北京航空航天大学飞行器设计与应用力学系

出　　处：《北京航空航天大学学报》2003年第2期95-98,共4页Journal of Beijing University of Aeronautics and Astronautics

摘　　要：为解决某型飞机加装固定式受油装置后引起的座舱噪声过大问题 ,通过空测摸清了飞行中噪声的变化规律 ,借助风洞试验等手段研究确定了噪声产生的机理 ,在此基础上提出了降噪改进措施 ,对受油管进行了修形改进设计 .Fixed refueling pipe added to a fighter induces an obvious increase of the cabin noise. In order to reduce the noise, the changing laws of the cabin noise was tested in flight, then the reason of noise increase was investigated by flow field visualization tests and turbulent flow measurements in wind tunnel. After the design of refueling pipe was modified according to the results of present study, the cabin noise was obviously reduced.

关 键 词：空中受油装置 战斗机 噪声控制 流场校测试验 受油管 

分 类 号：V228.17[航空宇航科学与技术—飞行器设计] TB535[理学—物理]