• Infrared and Laser Engineering
  • Vol. 52, Issue 12, 20230260 (2023)
Weibo Shi1, Haihao Sun1, Chunsheng Liu2, Shichang Liang1, and Anhua Shi1,*
Author Affiliations
  • 1Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
  • 2Beijing Institute of Electronic System Engineering, Beijing 100854, China
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    DOI: 10.3788/IRLA20230260 Cite this Article
    Weibo Shi, Haihao Sun, Chunsheng Liu, Shichang Liang, Anhua Shi. Analysis of the influence of aerodynamic heating in ascent stage on infrared radiation characteristics of high-speed aircraft in midcourse[J]. Infrared and Laser Engineering, 2023, 52(12): 20230260 Copy Citation Text show less
    Radiation energy exchange between aircraft and space environment
    Fig. 1. Radiation energy exchange between aircraft and space environment
    Geometric position relationship between target surface and pupil surface of detector
    Fig. 2. Geometric position relationship between target surface and pupil surface of detector
    Partial drawing of aircraft (Unit: mm)[19]
    Fig. 3. Partial drawing of aircraft (Unit: mm)[19]
    Comparison between the calculated temperature and the measured temperature of the flight test measuring point position
    Fig. 4. Comparison between the calculated temperature and the measured temperature of the flight test measuring point position
    Relative deviation of comparison between calculated temperature and measured temperature of flight test measuring point position
    Fig. 5. Relative deviation of comparison between calculated temperature and measured temperature of flight test measuring point position
    Assumes the geometric shape of aircraft (Unit: mm)
    Fig. 6. Assumes the geometric shape of aircraft (Unit: mm)
    Variation temperature of the typical position with time of flight under aerodynamic heating and sunlight
    Fig. 7. Variation temperature of the typical position with time of flight under aerodynamic heating and sunlight
    Variation temperature of the typical position with time of flight under sunlight without considering aerodynamic heating
    Fig. 8. Variation temperature of the typical position with time of flight under sunlight without considering aerodynamic heating
    The radiation intensity of 3-5 μm band changes with flight time
    Fig. 9. The radiation intensity of 3-5 μm band changes with flight time
    The radiation intensity of 8-12 μm band changes with time of flight
    Fig. 10. The radiation intensity of 8-12 μm band changes with time of flight
    Comparison of the variation of radiation intensity at 3-5 μm and 8-12 μm bands with time of flight
    Fig. 11. Comparison of the variation of radiation intensity at 3-5 μm and 8-12 μm bands with time of flight
    MaterialDensity/ kg·m–3Specific/ J·(kg·K)–1Thermal conductivity/ W·(m·K)–1
    Carbon-carbon composites17501172.30.83736
    Carbon-phenolic composites140012560.7536
    Insulating material2205500.019
    LF62640921125.6
    Table 1. Physical parameters of aircraft
    Weibo Shi, Haihao Sun, Chunsheng Liu, Shichang Liang, Anhua Shi. Analysis of the influence of aerodynamic heating in ascent stage on infrared radiation characteristics of high-speed aircraft in midcourse[J]. Infrared and Laser Engineering, 2023, 52(12): 20230260
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