• Infrared and Laser Engineering
  • Vol. 53, Issue 1, 20230176 (2024)
Rong Lv1, Qinglin Niu1, and Xiaobing Wang2
Author Affiliations
  • 1School of Mechanical and Electrical Engineering, North University of China, Taiyuan 030051, China
  • 2National Key Laboratory of Scattering and Radiation, Shanghai 200438, China
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    DOI: 10.3788/IRLA20230176 Cite this Article
    Rong Lv, Qinglin Niu, Xiaobing Wang. Numerical simulation of infrared radiation characteristics of near-space aircraft side jet due to angle of attack[J]. Infrared and Laser Engineering, 2024, 53(1): 20230176 Copy Citation Text show less
    References

    [1] Lee J W, Min B Y, Byun Y H, et al. Numerical analysis design optimization of lateral jet controlled missile[C]Proceedings of the 21st International Congress of Theetical Applied Mechanics, Warsaw, Pol, 2004, 145(2): 521.

    [2] Judson J. US, Lsrael''s Arrow3 missile put to the test in Alaska [EBOL]. (20190729) [20231009]. https:www.defensenews.compentagon20190728usisraelsarrow3missileputtothetestinalaska.

    [3] W Huang, W D Liu, S B Li, et al. Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows. Acta Astronautica, 73, 1-9(2012).

    [4] D A Dickmann, F K Lu. Shock/boundary-layer interaction effects on transverse jets in crossflow over a flat plate. Journal of Spacecraft and Rockets, 46, 1132-1141(2009).

    [5] K Choi, S Lee, K Oh, et al. Numerical investigation of jet interactions for a lateral thrust jet controlled interceptor operating at medium altitudes. International Journal of Aeronautical and Space Sciences, 21, 39-49(2020).

    [6] Dong Chai, Yangwang Fang, Weishi Peng, et al. Numerical investigation of lateral jet interaction effects on the hypersonic quasi-waverider vehicle. Journal of Aerospace Engineering, 229, 2671-2680(2015).

    [7] H B Ebrahimi. Numerical investigation of jet interaction in a supersonic freestream. Journal of Spacecraft and Rockets, 45, 95-103(2008).

    [8] A Gülhan, G Schütte, B Stahl. Experimental study on aerothermal heating caused by jet-hypersonic crossflow interaction. Journal of Spacecraft and Rockets, 45, 891-899(2008).

    [9] Tiesuo Gao, Tao Jiang, Mingsong Ding, et al. Numerical simulation of infrared radiation characteristics of flow over hypersonic interceptors. Infrared and Laser Engineering, 46, 85-92(2017).

    [10] Anhua Shi, Haiyan Li, Weibo SHI, et al. Infrared radiation feature of near space hypersonic cruise vehicle. Acta Armamentarii, 43, 796-803(2022).

    [11] Yatao Chen, Hongru Zheng, Xiang Ren, et al. Backward monte carlo method for simulating spectral radiation characteristics of boost-gliding vehicle. Aerospace Science and Technology, 132, 108087(2023).

    [12] Aoxiao Fuyang, Tao Jiang, Qingzong Liu, et al. Numerical simulation on radiation effect of hypersonic vehicle's hot gas jet. Infrared and Laser Engineering, 51, 20220023(2022).

    [13] Qinglin Niu, Zhichao Yuan, Biao Chen, et al. Infrared radiation characteristics of a hypersonic vehicle under time-varying angles of attack. Chinese Journal of Aeronautics, 32, 861-874(2019).

    [14] Qinglin Niu, Wenqiang Gao, Yiqiang Sun, et al. Investigation on infrared radiation signatures of under-expanded rocket exhaust plumes due to angle of attack. IEEE Access, 9, 113156-113168(2021).

    [15] Qinglin Niu, Sen Yang, Zhihong He, et al. Numerical study of infrared radiation characteristics of a boost-gliding aircraft with reaction control systems. Infrared Physics & Technology, 92, 417-428(2018).

    [16] D E Jensen, G A Jones. Reaction rate coefficients for flame calculations. Combustion and Flame, 32, 1-34(1978).

    [17] Modest M F. Radiative Heat Transfer [M]3rd ed, New Yk: Academic Press, 2013.

    [18] B Krakow, H J Babrov, G J Maclay, et al. Jordan, et al. Use of the Curtis–Godson approximation in calculations of radiant heating by inhomogeneous hot gases. Applied Optics, 5, 1791-1800(1966).

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

    [20] Sparrow E M, Radiation heat transfer[M]. London: Routledge, 2018.

    [21] P Gnemmi, P Gruhn, M Leplat, et al. Computation validation on lateral jet interactions at supersonic speeds. International Journal of Engineering Systems Modelling and Simulation, 5, 68-83(2013).

    [22] G Avital, Y Cohen, L Gamss, et al. Experimental and computational study of infrared emission from underexpanded rocket exhaust plumes. Journal of Thermophysics and Heat Transfer, 15, 377-383(2001).

    [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, Xiaobing Wang. Numerical simulation of infrared radiation characteristics of near-space aircraft side jet due to angle of attack[J]. Infrared and Laser Engineering, 2024, 53(1): 20230176
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