尾向可见明火大宽高比混合排气喷管红外抑制特性试验
Experimental investigation of infrared suppressing characteristics of rectangular nozzles with large aspect ratio
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摘要: 对5组不同宽高比(W/H=1~1)的圆转矩形收敛喷管模型(AR1~AR1) 在尾向可见明火时的红外辐射特性进行了试验研究,并与等出口面积的轴对称喷管(AR0)进行了比较,喷管模型为某型实际喷管缩比4.3倍得到的.研究发现,与轴对称喷管相比,大宽高比矩形喷管减小了红外源的辐射特征,起到了明显的红外抑制作用.在0°~90°范围内,所研究的喷管在3~5 μm波段上的红外辐射信号呈现随探测角度增大逐渐减小的规律.Abstract: The infrared suppressing characteristics of five rectangular convergent nozzles with different aspect ratios were investigated experimertey.The aspect ratio of the rectangular nozzles is 1,4,8,12,and 16,named AR1~AR16 respectively,while the axisymmetric nozzle is named AR0.The results indicate that infrared radiation from rectangular nozzle decreases with the increase of detection angle,and the magnitude of infrared radiation is smaller than axisymmetric one,and would accelerate with the rise of aspect ratio.
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[1] Dusa D J,Speir D W,Rowe R K.Advanced technology exhaust nozzle development[R].AIAA 83-1286. [2] 理查森 D.现代隐身飞机[M].北京:科学出版社,1991. [3] 郑礼宝.全尺寸二元喷管红外辐射特性研究[J].航空学报,2002,23(2):140-142.ZHEN Libao.Infrared emission from turbojet with two-dimensional nozzle[J].Acta Aeronautica Et Astronautica,2002,23(2):140-142. [4] 罗明东,吉洪湖,黄伟,等.涡扇发动机二元喷管的红外光谱辐射特性的实验研究[J].推进技术,2007,28(2):152-156.LUO Mingdong,JI Honghu,HUANG Wei,et al.Experiment on spectral infrared radiation characteristics of exhaust jet from 2D nozzle of turbofan engine[J].Journal of Propulsion Technology,2007,28(2):152-156. [5] 张勃,吉洪湖.大宽高比矩形喷管的射流与外流的掺混特性的数值研究[J].航空动力学报,2004,19(2):104-110.ZHANG Bo,JI Honghu.Numerical study of internal and external flow mixing for rectangular nozzles with large aspect ratio[J].Journal of Aerospace Power,2004,19(2):104-110. [6] 张勃,吉洪湖,罗明东,等,宽高比对尾向可见明火矩形喷管红外抑制特性影响研究[J].航空动力学报,2007,22(11):1820-1825.ZHANG Bo,JI Honghu,LUO Mingdong,et al.Investigation of the effect of aspect ratio to infrared suppressing characteristics of rectangular nozzles[J].Journal of Aerospace Power,2007,22(11):1820-1825. [7] Wallace R C.Apparatus for suppressing infrared radiation emitted from gas turbine engines[P].United Stated Patent,No.4800715.
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