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小偏距S弯二元喷管的红外辐射特性数值分析
引用本文:于明飞,吉洪湖,李宁,王浩,斯仁,刘健. 小偏距S弯二元喷管的红外辐射特性数值分析[J]. 航空动力学报, 2015, 30(9): 2080-2087. DOI: 10.13224/j.cnki.jasp.2015.09.005
作者姓名:于明飞  吉洪湖  李宁  王浩  斯仁  刘健
作者单位:1. 南京航空航天大学 能源与动力学院, 南京 210016;
摘    要:为了降低飞行器的红外辐射,适应发动机排气系统与飞机后机身的匹配,设计了一种非常规的S弯二元喷管,喷管出口中心线与发动机轴线不共线,有一个小偏距.在商业软件中计算该S弯二元喷管的温度场、速度场、压力场和组分浓度的分布,采用自主开发的红外软件,用反向蒙特卡罗法计算该喷管的红外辐射特性,并与基准轴对称喷管的计算结果进行对比,计算结果表明:采用小偏距S弯二元喷管后,能够对排气系统内部高温部件有一定的遮挡,对红外辐射特征有一定的抑制作用,最大能够降低33%的红外辐射. 

关 键 词:S弯二元喷管   小偏距   红外辐射   反向蒙特卡罗法   排气系统
收稿时间:2014-03-12

Numerical analysis on infrared radiation characteristics of two-dimensional S-nozzle with small offset
YU Ming-fei,JI Hong-hu,LI Ning,WANG Hao,SI Ren and LIU Jian. Numerical analysis on infrared radiation characteristics of two-dimensional S-nozzle with small offset[J]. Journal of Aerospace Power, 2015, 30(9): 2080-2087. DOI: 10.13224/j.cnki.jasp.2015.09.005
Authors:YU Ming-fei  JI Hong-hu  LI Ning  WANG Hao  SI Ren  LIU Jian
Affiliation:1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;2. Guizhou Aero-engine Research Institute, Aviation Industry Corporation of China, Guiyang 550081, China
Abstract:In order to reduce the infrared radiation of aircraft, and make the exhaust system match the aircraft afterbody, a kind of unconventional two-dimensional(2-D)S-nozzle was designed to suppress the infrared radiation characteristics. There was a small offset given that the nozzle's center line and the engine's axis were not collinear. Based on the distribution of temperature, pressure and species mass fraction of the two-dimensional S-nozzle obtained from CFD results, the infrared radiation characteristics of two-dimensional S-nozzle was calculated with reverse Monte-Carlo method, then analyzed and compared with axisymmetric nozzle. The results show that, the two-dimensional S-nozzle is capable of shielding the high temperature elements inside the exhaust system effectively, and the infrared radiation characteristics of the exhaust system can be further suppressed by 33%.
Keywords:2-D S-nozzle  small offset  infrared radiation  reverse Monte-Carlo method  exhaust system
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