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
Fig. 4. The single molecule spectral absorption coefficients for the 3-5 μm and 8-14 μm wavelength ranges based on HITRAN
Fig. 5. Error analysis of the spectral absorption coefficient for H2O
Fig. 6. Error analysis of the spectral absorption coefficient for CO2
Fig. 7. Error analysis of the spectral absorption coefficient for CO
Fig. 8. Single-molecule spectral absorption coefficients in the HITEMP database
Fig. 9. Error analysis of the spectral absorption coefficient for CO
Fig. 10. The computation of spectral radiation intensity for a one-dimensional non-isothermal homogeneous plate
Fig. 11. The spectral absorption coefficient and radiation intensity distribution of a mixed gas
Fig. 12. The absorption coefficient of a single molecule and the distribution of radiation intensity with wavenumber
Fig. 13. Absolute discrepancy between the single-molecule Planck average absorption coefficient and spectral radiation intensity
Fig. 14. Schematic diagram of the calculation domain of the exhaust system
Fig. 17. Analysis of the calculation results of infrared radiation imaging with small angle: (a) 0°; (b) 5°; (c) 10°; (d) 15°
Fig. 18. Comparison of calculated results of spectral radiation intensity at the front and rear
Fig. 19. The variation of integral radiation intensity with the azimuth angle
Fig. 20. The absolute error of the calculation results of the integral radiation intensity of the convergent nozzle under different azimuth angles
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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
Category: Infrared
Received: Feb. 16, 2025
Accepted: --
Published Online: Aug. 29, 2025
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