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Fig. 5. Temperature of surface of aircraft and surrounding airflow. (a) Side view; (b) top view. Aircraft velocity was Mach 1.5 and altitude was 5000 m.
Kim, Taehwan et al. “Susceptibility of combat aircraft modeled as an anisotropic source of infrared radiation.” IEEE Transactions on Aerospace and Electronic Systems 52 (2016): 2467-2476. }
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