Infrared and Laser Engineering, Volume. 52, Issue 4, 20220621(2023)

Quantitative analysis of the uncertainty of infrared radiation signature of rocket exhaust plume caused by incoming flow

Zhiru Xiao1, Qinglin Niu1, Zhenhua Wang2, and Shikui Dong3
Author Affiliations
  • 1College of Mechatronic Engineering, North University of China, Taiyuan 030051, China
  • 2Science and Technology on Optical Radiation Laboratory, Beijing Institute of Environmental Features, Beijing 100854, China
  • 3Key Laboratory of Aerospace Thermophysics of MIIT, Harbin Institute of Technology, Harbin 150001, China
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    Figures & Tables(10)
    Computational domain and grids
    Comparison of infrared radiation intensity spectral of flare between calculation and reference results
    Contours of flow field parameters in baseline case
    Radiation intensity of Atlas-IIA plume at H=15 km
    Spectral radiation intensity uncertainty band and uncertainty
    Main Sobol index of free stream parameters to spectral intensity: (a) velocity, (b) pressure, (c) temperature, and (d) angle of attack
    Sobol index of coupling effect of free stream parameters to spectral intensity
    Sobol index of free stream parameters to in-band spectral intensity: (a) 3-5 μm band, (b) 2.5-3.2 μm band, (c) 2.8-3.0 μm band, and (d) 4.35-4.65 μm band
    • Table 1. Parameters of free stream flow and nozzle exit [15]

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      Table 1. Parameters of free stream flow and nozzle exit [15]

      ParameterFree streamNozzle
      U/m·s−1545.52 960
      P/Pa 12 11268 850
      T/K 216.72 230
      H20.000 0000.012 194
      O20.233 1540.000 028
      H2O 0.000 0000.272 437
      H0.000 0000.000 127
      OH0.000 0000.000 797
      N20.766 3880.000 000
      CO0.000 0000.412 125
      CO20.000 4580.302 293
    • Table 2. Statistical properties of in-band radiance intensity

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      Table 2. Statistical properties of in-band radiance intensity

      BandMean value/W·sr−1Standard deviation/W·sr−1Uncertainty
      19.83×1066.62×1056.70%
      21.05×1076.77×1056.50%
      33.72×1062.55×1056.90%
      43.85×1063.50×1059.10%
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    Zhiru Xiao, Qinglin Niu, Zhenhua Wang, Shikui Dong. Quantitative analysis of the uncertainty of infrared radiation signature of rocket exhaust plume caused by incoming flow[J]. Infrared and Laser Engineering, 2023, 52(4): 20220621

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    Paper Information

    Category: Infrared technology and application

    Received: Aug. 31, 2022

    Accepted: --

    Published Online: Jul. 4, 2023

    The Author Email:

    DOI:10.3788/IRLA20220621

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