Volume 44 Issue 6
Aug.  2015
Turn off MathJax
Article Contents

Gao Xiang, Yang Qingzhen, Shi Yongqiang, Wang Yun, Yang Huicheng. Numerical simulation of radiation intensity of double S-shaped exhaust system with different outlet shapes[J]. Infrared and Laser Engineering, 2015, 44(6): 1726-1732.
Citation: Gao Xiang, Yang Qingzhen, Shi Yongqiang, Wang Yun, Yang Huicheng. Numerical simulation of radiation intensity of double S-shaped exhaust system with different outlet shapes[J]. Infrared and Laser Engineering, 2015, 44(6): 1726-1732.

Numerical simulation of radiation intensity of double S-shaped exhaust system with different outlet shapes

  • Received Date: 2014-10-13
  • Rev Recd Date: 2014-11-17
  • Publish Date: 2015-06-25
  • Several double-S nozzles with different outlet shapes were designed based on an axis-symmetric nozzle to analyze influence of the outlet shape on the infrared radiation(IR) characteristics of exhaust system. The curvature regulation method and mass-flow matching principle were adopted in the design. The distribution of the characteristics of flow field and mass fraction of six exhaust system models were obtained by CFD. The IR characteristics of these models were calculated by reverse Monte-Carlo method (RMCM), and then IR intensity space distribution of the rear hemisphere, radiation brightness distribution and the lock distance of the rear hemisphere were researched. The results show that, the double S-shaped nozzle can reduce the infrared signal of target effectively. The outlet shape can affect the IR characteristics of exhaust system. The models with trapezoid outlet shape has significantly lower IR intensity than the double S-shaped nozzles with other outlet shapes, and can reduce the peak of IR intensity at least 70% compared with the axis-symmetric nozzle. Reducing trapezoid's bottom angle can enhance the infrared suppression effect, and appropriate outlet shape can further suppress the IR intensity of exhaust system within acceptable thrust loss.
  • [1]
    [2] Haulman D L. USAF manned aircraft combat Losses 1990-2002 [R]. AD A434084, 2002.
    [3] Mahulikar S P, Sonawance H R, Rao G A. Infrared signature studies of aero space vehicles[J]. Progress in Aerospace Sciences, 2007, 43(7): 218-245.
    [4]
    [5]
    [6] Marlene Johansson. Propulsion Integration in an UAV[R].AIAA 2006-2834, 2006.
    [7]
    [8] Liu Changchun, Ji Honghu, Huang Wei, et al. Numerical simulation on infrared radiation characteristics of serpentine 2-D nozzle[J]. Journal of Aerospace Power, 2013, 28(7): 1482-1488. (in Chinese) 刘常春, 吉洪湖, 黄伟, 等. 一种双S弯二元喷管的红外辐射特性数值研究[J].航空动力学报, 2013, 28(7): 1482-1488.
    [9] Zhang Yechuan, Wang Zhanxue, Shi Jingwei, et al. Analysis on flow and infrared radiation characteristics of double S-nozzle [J]. Journal of Aerospace Power, 2013, 28(11): 2468-2474. (in Chinese) 章叶川, 王占学, 史经纬, 等. 双S弯喷管流动特性及红外辐射特性分析[J].航空动力学报, 2013, 28(11): 2468-2474.
    [10]
    [11] Li Yuefeng, Yang Qingzhen. Huan Xia, et al. Influence on radar cross-section of S-shaped two dimensional convergent nozzles with different outlet width-height ratios[J]. Journal of Aerospace Power, 2014, 29(3): 645-651. (in Chinese) 李岳锋, 杨青真, 环夏, 等. 出口宽高比对S形二元收敛喷管雷达散射截面的影响[J]. 航空动力学报, 2014, 29(3): 645-651.
    [12]
    [13]
    [14] Li Wei, Zhang Bo, Wang Fei, et al. Numerical simulation on infrared radiation characteristics of round to rectangular nozzles with different chevrons considering engine components[J]. Journal of Aerospace Power, 2014, 29(8): 1810-1816. (in Chinese) 李伟, 张勃, 王飞, 等. 不同锯齿对圆转矩形喷管红外辐射特征影响数值模[J]. 航空动力学报, 2014, 29(8): 1810-1816.
    [15]
    [16] Li Yuefeng, Yang Qingzhen, Li Xiang, et al. RCS characteristic of S-shaped nozzle with different outlet shapes[J]. Journal of Aerospace Power, 2013, 28(12): 2671-2677. (in Chinese) 李岳锋, 杨青真, 李翔, 等. 不同出口形状S形喷管的RCS特性[J]. 航空动力学报, 2013, 28(12): 2671-2677.
    [17]
    [18] Gao Xiang, Yang Qingzhen, Mu Hongrui. Numerical simulation of radar scattering characteristics for 2-D nozzles with different aspect ratios[J]. Journal of Propulsion Technology, 2014, 35(6): 735-741. (in Chinese) 高翔, 杨青真, 母鸿瑞. 不同宽高比的二元喷管电磁散射特性数值研究[J]. 推进技术, 2014, 35(6): 735-741.
    [19] Chen Lihai, Yang Qingzhen, Chen Lingling. Numerical simulation of RCS for 2D convergent nozzle with different trailing edges[J]. Journal of Aerospace Power, 2012, 27(3): 513-520. (in Chinese) 陈立海, 杨青真, 陈玲玲. 不同喷口修形的二元收敛喷管RCS数值模拟[J]. 航空动力学报, 2012, 27(3): 513-520.
    [20]
    [21]
    [22] Huang Wei, Ji Honghu, Si Ren. Infrared characteristics calculating of turbofan engine exhaust system[J]. Journal of Propulsion Technology, 2010, 31(6): 745-772. (in Chinese) 黄伟, 吉洪湖, 斯仁. 涡扇发动机排气系统红外特征[J]. 推进技术, 2010, 31(6): 745-772.
    [23] Wang K C. Prediction of rocket plume radioactive heating using backward monte-carlo method[R]. AIAA 93-0137, 1993.
    [24]
    [25] Chen Lihai. Numerical simulation on the infrared radiation characteristics of exhaust system of the aircraft[D]. Xi'an:Northwestern Polytechnical University, 2013.
    [26]
    [27] Rao G A, Mahulikar S P. Effect of atmospheric transmission and radiance on aircraft infrared signatures[J]. Journal of Aircraft, 2005, 42: 1046-1054.
  • 加载中
通讯作者: 陈斌, bchen63@163.com
  • 1. 

    沈阳化工大学材料科学与工程学院 沈阳 110142

  1. 本站搜索
  2. 百度学术搜索
  3. 万方数据库搜索
  4. CNKI搜索

Article Metrics

Article views(454) PDF downloads(128) Cited by()

Related
Proportional views

Numerical simulation of radiation intensity of double S-shaped exhaust system with different outlet shapes

  • 1. School of Power and Energy,Northwestern Polytechnical University,Xi'an 710129,China

Abstract: Several double-S nozzles with different outlet shapes were designed based on an axis-symmetric nozzle to analyze influence of the outlet shape on the infrared radiation(IR) characteristics of exhaust system. The curvature regulation method and mass-flow matching principle were adopted in the design. The distribution of the characteristics of flow field and mass fraction of six exhaust system models were obtained by CFD. The IR characteristics of these models were calculated by reverse Monte-Carlo method (RMCM), and then IR intensity space distribution of the rear hemisphere, radiation brightness distribution and the lock distance of the rear hemisphere were researched. The results show that, the double S-shaped nozzle can reduce the infrared signal of target effectively. The outlet shape can affect the IR characteristics of exhaust system. The models with trapezoid outlet shape has significantly lower IR intensity than the double S-shaped nozzles with other outlet shapes, and can reduce the peak of IR intensity at least 70% compared with the axis-symmetric nozzle. Reducing trapezoid's bottom angle can enhance the infrared suppression effect, and appropriate outlet shape can further suppress the IR intensity of exhaust system within acceptable thrust loss.

Reference (27)

Catalog

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return