• Infrared and Laser Engineering
  • Vol. 53, Issue 9, 20240248 (2024)
Yunsong FENG1,2, Tong WANG1,2, Siyu WANG1,2, Wei JIN1,2..., Yuanxin SHANG1,2 and Changqi ZHOU1,2|Show fewer author(s)
Author Affiliations
  • 1State Key Laboratory of Pulsed Power Laser Technology, National University of Defense Technology, Hefei 230037, China
  • 2Infrared and Low Temperature Plasma Key Laboratory of Anhui Province, National University of Defense Technology, Hefei 230037, China
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    DOI: 10.3788/IRLA20240248 Cite this Article
    Yunsong FENG, Tong WANG, Siyu WANG, Wei JIN, Yuanxin SHANG, Changqi ZHOU. Study on infrared radiation characteristics of rotorcraft based on Monte Carlo method[J]. Infrared and Laser Engineering, 2024, 53(9): 20240248 Copy Citation Text show less
    Geometric model of small rotorcraft
    Fig. 1. Geometric model of small rotorcraft
    Surface meshing
    Fig. 2. Surface meshing
    Far-infrared thermal images of rotorcraft under different working conditions. (a) Static and no load; (b) 10-minute flight and no load; (c) 10-minute flight and load 100 g
    Fig. 3. Far-infrared thermal images of rotorcraft under different working conditions. (a) Static and no load; (b) 10-minute flight and no load; (c) 10-minute flight and load 100 g
    Gridded spherical receiving surface
    Fig. 4. Gridded spherical receiving surface
    Flow chart of calculating infrared radiation by Monte Carlo method
    Fig. 5. Flow chart of calculating infrared radiation by Monte Carlo method
    Spatial distribution of far-infrared radiation intensity of rotorcraft under different working conditions. (a) Static and no load; (b) 10-minute flight and no load
    Fig. 6. Spatial distribution of far-infrared radiation intensity of rotorcraft under different working conditions. (a) Static and no load; (b) 10-minute flight and no load
    Curve of radiation intensity with zenith angle θ while \begin{document}$\varphi {\text{ = 90}}{\text{.}}{{\text{9}}^{\text{o}}}$\end{document}
    Fig. 7. Curve of radiation intensity with zenith angle θ while Unknown environment 'document'
    Curve of radiation intensity with circumferential angle φ while θ = 78.3°
    Fig. 8. Curve of radiation intensity with circumferential angle φ while θ = 78.3°
    Flight time/minLoad/gRegionTemperature/℃
    00Electric machinery28.3
    Battery31.5
    Fuselage29.6
    100Electric machinery46.3
    Battery38.3
    Fuselage33.1
    10100Electric machinery54.6
    Battery44.5
    Fuselage33.4
    Table 1. Temperature values of each part of the rotorcraft under different working conditions
    Yunsong FENG, Tong WANG, Siyu WANG, Wei JIN, Yuanxin SHANG, Changqi ZHOU. Study on infrared radiation characteristics of rotorcraft based on Monte Carlo method[J]. Infrared and Laser Engineering, 2024, 53(9): 20240248
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