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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    Figures & Tables(21)
    The model of baseline axisymmetric exhaust system combined with aircraft rear body
    The model of 2 D exhaust system combined with aircraft rear body
    Schematic diagram of FSGV and cone
    The model of 2D exhaust system with FSGV and combined with aircraft rear body
    Schematic diagram of flow field computational domain
    Grid of flow field and wall in combined model
    Grid independence verification
    Schematic diagram of 2D exhaust system combined with rear body model detection surface
    Static pressure distribution on the rear body external surface
    Temperature field distribution on the middle section of three combined models
    Temperature along the wall of the C-D nozzle section of three combined models
    Mass fraction of CO2 on the middle section of three combined models
    Comparison of radiation intensity of three combined model
    Radiation intensity of main component of the baseline axisymmetric exhaust system combined with rear body model
    Radiation intensity of main component on horizontal detection surface of the 2D exhaust system combined with rear body model
    Radiation intensity of main component on horizonta detection surface of the 2D exhaust system with FSGV combined with rear body model
    The radiation intensity of FSGV when the vane is cooling
    Comparison of radiation intensity of 2D exhaust system with FSGV and combined with rear body model when the vane is cooling
    • Table 1. Boundary conditions

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      Table 1. Boundary conditions

      $ {P_t}/{P_0} $$ {T_t} $(K) ${Y_{\rm C{ O_2} } }$${Y_{ \rm {H_2}O} }$${Y_{\rm CO} }$
      Core inlet4.648500.0660.0250.0001
      Bypass inlet4.60350
    • Table 2. Flow and thrust characteristic

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      Table 2. Flow and thrust characteristic

      Baseline axisymmetric exhaust system 2D exhaust system2D exhaust system with FSGV
      Cd0.9910.9780.962
      Cf0.9760.9730.96
    • Table 3. Resistance of rear body external surface

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      Table 3. Resistance of rear body external surface

      Pressure resistance/NViscous resistance/NTotal resistance/N
      Baseline axisymmetric exhaust system773.008289.1711062.172
      2D exhaust system810.568298.3501108.918
      2D exhaust system with FSGV819.465289.1721108.638
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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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