Infrared and Laser Engineering, Volume. 51, Issue 9, 20210965(2022)

Numerical study of fluid flow, heat transfer and infrared signature of 2D exhaust system model with full shielded guide vane combined with rear body

Wen Cheng1, Honghu Ji1, Xiaojuan Shi1, and Hao Wang2
Author Affiliations
  • 1College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • 2Yangzhou Collaborative Innovation Research Institute CO.LTD, Yangzhou 225000, China
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    References(16)

    [1] Honghu Ji. Fundamental issues of aircraft / engine integration for low observability. Aerospace Propulsion, 67-71(2018).

    [2] Renyu Fan, Jingzhou Zhang, Yong Shan. Effects of sheltering baffles on the infrared radiation characteristics of two-dimensional nozzles. Journal of Aeronautics and Dynamics, 26, 343-348(2011).

    [3] Jun Chen, Honghu Ji, Changchun Liu. The experimental study of infrared suppression of 2D plug nozzle with cooling structure. Gas Turbine Test and Research, 32, 18-23, 46(2019).

    [4] Feifei Cao, Honghu Ji, Mingfei Yu, et al. Effects of low emissivity material coating site on wall temperature and infrared characteristics of exhaust system. Infrared and Laser Engineering, 49, 20190131(2020).

    [5] Hongwei Deng, Wendong Jin, Liuzeng Ye, et al. Numerical simulation of two-dimensional nozzle and analysis of its stealth technology. Aeronautical Science and Technology, 1, 45-47(2012).

    [6] Changchun Liu, Honghu Ji. Experiment on infrared radiation characteristics of S shaped 2D nozzle. Journal of Aerospace Power, 34, 1493-1500(2019).

    [7] Jingzhou Zhang, Xu Wang, Yong Shan. Effects of plug rear-body film cooling on infrared radiation and aerodynamic performance of axisymmetric plug nozzle. Journal of Aeronautics, 36, 2601-2608(2015).

    [8] Zhangbin Huang, Liu Guan, Xiaoxia Li, et al. Numerical simulation of radiation characteristics of aircraft exhaust systems with different nozzles. Infrared Technology, 43, 587-591(2021).

    [9] Xiaoyu Hu. VAATE,US' new advanced turbine engine technology development program. International Aviation, 40-42(2007).

    [10] Yong Shan, Jingzhou Zhang, Wanren Shao, et al. Experiment on aerodynamic and infrared radiation characteristics of the film cooling center-body exhaust system for a turbofan engine. Journal of Aeronautics and Dynamics, 27, 9-15(2012).

    [11] Xiaojuan Shi, Honghu Ji. Numerical investigation of influence of two-dimensional convergent and divergent nozzle's design parameters on infrared characteristics. Journal of Aerospace Power, 35, 944-955(2020).

    [12] Hao Wang, Honghu Ji, Xueyi Sang, et al. Effects of fully shielded guiding strut on infrared signatures of exhaust system. Journal of Aerospace Power, 35, 2078-2088(2020).

    [13] R E Martens. F-15 Nozzle/afterbody integration. Journal of Aircraft, 13, 327-333(1976).

    [14] [14] Mattingly J D, Heiser W H, Pratt D T, et al. Aircraft Engine Design[M]. Reston: American Institute of Aeronautics Astronautics, 2002.

    [15] Yuefeng Li, Zhenqing Yang, Zhigang Sun. Design of super-elliptic S-shaped inlet and analysis of aerodynamic performance. Computer Simulation, 28, 82-85, 96(2011).

    [16] Na Li, Honghu Ji. Configuration design method of high performance two-dimensional convergent nozzle. Aero Engine, 45, 1-6(2019).

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    Wen Cheng, Honghu Ji, Xiaojuan Shi, Hao Wang. Numerical study of fluid flow, heat transfer and infrared signature of 2D exhaust system model with full shielded guide vane combined with rear body[J]. Infrared and Laser Engineering, 2022, 51(9): 20210965

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    Paper Information

    Category: Infrared technology and application

    Received: Dec. 16, 2021

    Accepted: --

    Published Online: Jan. 6, 2023

    The Author Email:

    DOI:10.3788/IRLA20210965

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