Volume 29 Issue 2
Feb.  2014
Turn off MathJax
Article Contents
LIU Jian, GONG Yu, JI Hong-hu. Fighter's infrared characteristics between 8 and 14μm and infrared stealth effect of low emissivity materials[J]. Journal of Aerospace Power, 2014, 29(2): 259-267. doi: 10.13224/j.cnki.jasp.2014.02.003
Citation: LIU Jian, GONG Yu, JI Hong-hu. Fighter's infrared characteristics between 8 and 14μm and infrared stealth effect of low emissivity materials[J]. Journal of Aerospace Power, 2014, 29(2): 259-267. doi: 10.13224/j.cnki.jasp.2014.02.003

Fighter's infrared characteristics between 8 and 14μm and infrared stealth effect of low emissivity materials

doi: 10.13224/j.cnki.jasp.2014.02.003
  • Received Date: 2012-12-26
  • Publish Date: 2014-02-28
  • The infrared integral radiant intensity of a typical fighter within the waveband between 8μm and 14μm and its detection range detected by infrared search/tracking system was calculated by taking into account the influence of the atmospheric transmissivity. The infrared stealth effect of the fighter with use of low emissivity materials was also analyzed. The flow field was calculated by Flunt software,while the infrared radiation characteristics and detection range were simulated by using self-developed software NUAA-IRSE. The results show that the infrared integral radiant intensity increases with the increasing of circumference angle and pitch angle. When applying low emissivity materials, the infrared integral radiant intensity decreases in all directions, leading to an improved infrared stealth effect.

     

  • loading
  • [1]
    Nelson H P, Tucker E O.Infrared emission from jet engine exhaust plume[J].AIAA 86-0465, 1986.
    [2]
    Rao G A, Mahulikar S P.Aircraft powerplant and plume infrared signature modelling and analysis[J].AIAA 2005-211, 2005.
    [3]
    Mahulikar S P, Sonawane H R, Rao G A.Infrared signature studies of aerospace vehicles[J].Progress in Aerospace Science, 2007, 43(7/8):218-245.
    [4]
    吕建伟, 王强.飞行器表面温度和发射率分布对红外辐射特征的影响[J].光电工程, 2009, 36(2):50-54. LV Jianwei, WANG Qiang.Effect of temperature and emissivity of aircraft skin on infrared radiation characteristics[J].Opto-Electronic Engineering, 2009, 36(2):50-54.(in Chinese)
    [5]
    LU Jianwei, WANG Qiang.Aircraft-skin infrared radiation characteristics modeling and analysis[J].Chinese Journal of Aeronautics, 2009, 22(5):493-497.
    [6]
    施小娟.涡扇发动机收敛喷管红外辐射特征及引射抑制技术研究[D].南京:南京航空航天大学, 2007. SHI Xiaojuan.Investigation of infrared radiation ch-aracteristics of convergent nozzle in turbofan engine and ejector's suppressing technology[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2007.(in Chinese)
    [7]
    施小娟, 吉洪湖, 罗明东.发动机背负式安装无人机的排气系统红外特征的计算研究[J].航空动力学报, 2008, 23(4):651-656. SHI Xiaojuan, JI Honghu, LUO Mingdong.Numerical simulation of infrared radiation characteristics for exhaust system of an UAV with engine installed on the back of the fuselage[J].Journal of Aerospace Power, 2008, 23(4):651-656.(in Chinese)
    [8]
    冯晓星, 吉洪湖, 斯仁.战斗机3~5μm波段红外特征空间分布及低发射率材料隐身效果分析[J].红外技术, 2011, 33(7):389-405. FENG Xiaoxing, JI Honghu, SI Ren.Numerical study on spatial distribution of 3~5μm infrared signature and stealth effect of low emissivity material for fighter aircraft[J].Infrared Technology, 2011, 33(7):389-405.(in Chinese)
    [9]
    胡娅萍, 吉洪湖, 白涛涛.湍流模型对发动机排气系统流场和红外辐射特征计算的影响[J].航空动力学报, 2012, 27(11):2414-2420. HU Yaping, JI Honghu, BAI Taotao.Effect of turbulence models on numerical simulation of flow and infrared radiation characteristics of aero-engine exhaust system[J].Journal of Aerospace Power, 2012, 27(11):2414-2420.(in Chinese)
    [10]
    杜胜华, 龚加明, 夏新林.某飞行器红外辐射特性研究[J].红外与激光工程, 2008, 37(suppl.2):432-436. DU Shenghua, GONG Jiaming, XIA Xinlin.Infrared characteristics of a spacecraft[J].Infrared and Laser Engineering, 2008, 37(suppl.2):432-436.(in Chinese)
    [11]
    夏新林, 艾青, 任德鹏.飞机蒙皮红外辐射的瞬态温度场分析[J].红外与毫米波学报, 2007, 26(3):174-177. XIA Xinlin, AI Qing, REN Depeng.Analysis on the transient temperature-fields for infrared radiation of aircraft skin[J].Journal of Infrared Millim Waves, 2007, 26(3):174-177.(in Chinese)
    [12]
    罗明东, 吉洪湖, 黄伟.非加力涡轮发动机排气系统红外辐射强度的数值计算[J].航空动力学报, 2007, 22(10):1609-1616. LUO Mingdong, JI Honghu, HUANG Wei.Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning[J].Journal of Aerospace Power, 2007, 22(10):1609-1616.(in Chinese)
    [13]
    黄伟, 吉洪湖.加力式涡扇发动机非加力状态部件红外辐射分析[J].航空动力学报, 2011, 26(1):48-53. HUANG Wei, JI Honghu.Analysis of components infrared radiation of afterburning turbofan engine under non-afterburning condition[J].Journal of Aerospace Power, 2011, 26(1):48-53.(in Chinese)
    [14]
    陈玻若.红外系统[M].北京:兵器工业出版社, 1995.
    [15]
    张敬贤, 李玉丹, 金伟其.微光与红外成像技术[M].北京:北京理工大学出版社, 1995.
  • 加载中

Catalog

    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 (2152) PDF downloads(1148) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return