Infrared and Laser Engineering, Volume. 49, Issue 4, 0404002(2020)
Radiative transmission property of infrared window in hypersonic vehicle
Fig. 2. Flight trajectory (above) and attack angle and
Fig. 4. Spectral absorption coefficient of sapphire due to variety of wavelength and temperature
Fig. 5. Simulation results of adiabatic plate boundary layer friction coefficient comparing with ideal results due to variety of
Fig. 6.
Fig. 7.
Fig. 9. Minimum difference of target and background temperature recognizable by IR detector distribution at different time
Fig. 10. Volume average temperature and maximum temperature of sapphire at
Fig. 11. Δ
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Yihan Li, Haiyang Hu, Qiang Wang. Radiative transmission property of infrared window in hypersonic vehicle[J]. Infrared and Laser Engineering, 2020, 49(4): 0404002
Received: Dec. 6, 2019
Accepted: --
Published Online: May. 27, 2020
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