Infrared and Laser Engineering, Volume. 54, Issue 7, 20250110(2025)

Research on infrared radiation characteristics of high-temperature exhaust system of aircraft based on improved Monte Carlo method

Xiying WANG1, Donghang JIANG2, Zeyu ZHU2, Baohai GAO2, Hong QI2, and Yatao REN2
Author Affiliations
  • 1Aero Engine Academy of China, Beijing 101304, China
  • 2School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
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    Figures & Tables(21)
    Schematic diagram of LOS
    Ray tracing model of RMC in participating media
    Molecular line intensity distribution of HITRAN
    The single molecule spectral absorption coefficients for the 3-5 μm and 8-14 μm wavelength ranges based on HITRAN
    Error analysis of the spectral absorption coefficient for H2O
    Error analysis of the spectral absorption coefficient for CO2
    Error analysis of the spectral absorption coefficient for CO
    Single-molecule spectral absorption coefficients in the HITEMP database
    Error analysis of the spectral absorption coefficient for CO
    The computation of spectral radiation intensity for a one-dimensional non-isothermal homogeneous plate
    The spectral absorption coefficient and radiation intensity distribution of a mixed gas
    The absorption coefficient of a single molecule and the distribution of radiation intensity with wavenumber
    Absolute discrepancy between the single-molecule Planck average absorption coefficient and spectral radiation intensity
    Schematic diagram of the calculation domain of the exhaust system
    The temperature distribution of the exhaust system
    The pressure distribution of the exhaust system
    Analysis of the calculation results of infrared radiation imaging with small angle: (a) 0°; (b) 5°; (c) 10°; (d) 15°
    Comparison of calculated results of spectral radiation intensity at the front and rear
    The variation of integral radiation intensity with the azimuth angle
    The absolute error of the calculation results of the integral radiation intensity of the convergent nozzle under different azimuth angles
    • Table 1. Comparison of various versions of the HITRAN/HITEMP databases

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      Table 1. Comparison of various versions of the HITRAN/HITEMP databases

      Molecular database versionHITRANHITEMP
      200820122016202020102019
      AllNmolecular4247495558
      Nline56728637400447111277831113758230125705570135305134
      H2ONiso667766
      3-5 μmN148371248026581300411584551015845510
      Si /10 −208.75708.88398.85228.85218.75758.7575
      8-14 μmN114963668777282061910314119103141
      Si/ 10 −216.71346.73836.71836.71356.71376.7137
      CO2Niso910121277
      3-5 μmN27272910604112258511965628862612886261
      Si / 10 −161.00611.01181.01221.01221.00701.0070
      8-14 μmN22969443294544734999815614321561432
      Si / 10 −191.56081.58341.56521.56521.58391.5839
      CONiso666666
      3-5 μmN59479479609602363562008
      Si/ 10 −171.00991.00991.01091.01091.00991.0315
      8-14 μmN5----389820024
      Si/ 10 −99----0.0738340.23564
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    Xiying WANG, Donghang JIANG, Zeyu ZHU, Baohai GAO, Hong QI, Yatao REN. Research on infrared radiation characteristics of high-temperature exhaust system of aircraft based on improved Monte Carlo method[J]. Infrared and Laser Engineering, 2025, 54(7): 20250110

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    Paper Information

    Category: Infrared

    Received: Feb. 16, 2025

    Accepted: --

    Published Online: Aug. 29, 2025

    The Author Email:

    DOI:10.3788/IRLA20250110

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