Infrared and Laser Engineering, Volume. 52, Issue 7, 20220810(2023)

Numerical simulation of infrared radiation characteristics of the B-2-like aircraft

Rong Lv1, Qinglin Niu1, and Shikui Dong2
Author Affiliations
  • 1School of Mechanical and Electrical Engineering, North University of China, Taiyuan 030051, China
  • 2Key Laboratory of Aerospace Thermophysics of MIIT, Harbin Institute of Technology, Harbin 150001, China
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    References(23)

    [1] S Myong-hwan, J Jonghee, L Joon, et al. Stealth aircraft technology and future air warfare. Journal of the Korea Institute of Military Science and Technology, 22, 81-92(2019).

    [2] Xiaochun Xue, Xuehua Wang. The development study of stealth and antistealth. Modern Defence Technology, 32, 60-65(2004).

    [4] Jie Lin, Yong Jiang, Haobai Fang, et al. Modeling and analysis on self-Infrared radiation characteristics of whole aircraft skin. Infrared Technology, 34, 286-291(2012).

    [6] Dingguo Xu, Weilin Feng, Jianhua Sang. IR characteristics of aircraft aft fuselage skin. Infrared and Laser Engineering, 42, 7-13(2013).

    [7] Qiangang Zheng, Zhigui Xu, Yong Wang, et al. Overall optimization design of high temperature components cooling coefficient for lower infrared turbofan engine. Infrared Physics & Technology, 102, 102990(2019).

    [8] Fengming Wang, Yongmei Wang, Lei Zhang, et al. The development analysis to the powerplants for the long-range strategic bombers. Aerospace Power, 65-69(2020).

    [9] [9] Lian X C, Wu H. Principle of Aeroengine[M]. Xi''an: Nthwestern Polytechnical University Press, 2005. (in Chinese)

    [11] [11] Ludwig C B, Malkmus W, Reardon J E, et al. Hbook of infrared radiation from combustion gases, NASASP3080[R]. Alabama: NASA, 1973.

    [12] [12] Tan H P, Xia X L, Liu L H. Numerical Computation f Numerical Calculation of Infrared Radiation Properties Transmission Computational Radiation[M]. Harbin: Harbin Institute of Technology Press, 2006. (in Chinese)

    [13] Lei Mu, Yu Ma, Zhihong He, et al. Radiation characteristics simulation of non -equilibrium flow field around the hypersonic blunted cone. Journal of Engineering Thermophysics, 33, 1958-1962(2012).

    [14] [14] Chen Y J. Threedimensional reconstruction acteristic analysis of B2 flyingwing bomber[D]. Nanjing: Nanjing University of Aeronautics Astronautics, 2017. (in Chinese)

    [15] Xianqiao Wen. Discussion on generalities of “B-2” stealth strategic bomber. Modern Defence Technology, 29, 1-4(2001).

    [16] [16] Zhang W. Aircraft Engine[M]. Beijing: Aviation Industry Press, 2008. (in Chinese)

    [19] Pingyang Wang, Huier Cheng, Weihua Yang. Simulation of nozzle flow of two-component attitude control engine with DSMC method. Journal of Propulsion Technology, 112-114, 165(2003).

    [20] [20] Keenan J, Cler G. Simulation of ablation in earth atmospheric entry[C]28th Thermophysics Conference, 1993: 2789.

    [22] Xiao Yang, Qinglin Niu, Zhihong He, et al. Analysis of infrared radiation characteristics and detectability of HTV-2-like hypersonic gliding aircrafts. Acta Optica Sinica, 37, 20400(2017).

    [23] Qinglin Niu, Wenqiang Gao, Yiqiang Sun, et al. Study on influence of high-energy explosive components on infrared radiation signature of air to air missile plume. Journal of Ordnance Equipment Engineering, 42, 1-7(2021).

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    Rong Lv, Qinglin Niu, Shikui Dong. Numerical simulation of infrared radiation characteristics of the B-2-like aircraft[J]. Infrared and Laser Engineering, 2023, 52(7): 20220810

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    Paper Information

    Category: Infrared technology and application

    Received: Nov. 8, 2022

    Accepted: --

    Published Online: Aug. 16, 2023

    The Author Email:

    DOI:10.3788/IRLA20220810

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