[4] Cross E F. Windowheating effects on airbne infrared system calibration [C]Proceedings of SPIE, 1992, 1762: 576−583.
[6] Yahui Wang, 王亚辉, 王强, Qiang Wang, Bochuan Zhang, 张伯川. Evaluation method for aero-thermo-radiation effect of IR window. Infrared and Laser Engineering, 45, 0404002(2016).
[7] 王惠, Hui Wang, Fanyang Dang, 党凡阳, Rongda Zhang, 张荣达. Influence of thickness of hemispherical dome on aerodynamic thermal radiation. Infrared and Laser Engineering, 47, 153-158(2018).
[8] Pond J E, Welch C T, Sutton G W. Sidemounted IR window aerooptic aerothermal analysis [C]Proceedings of SPIE, 1999, 3705:266−275.
[9] Coiro E, Chatelard C, Dur G, et al. Experimental validation of an aircraft infrared signature code f commercial airliners[C]Aiaa Thermophysics Conference, 2006: 491495.
[10] Zhang S, Fang C, Hong L. Integrated fluidthermalstructural analysis f predicting aerothermal environment of hypersonic vehicles[C]Aerospace Sciences Meeting, 2013.
[12] Modest M F. Radiative Heat Transfer[M]. 3rd ed. San Diego: Academic Press, 2013.
[15] C G Speziale, E C Anderson, R Abid. A critical evaluation of two-equation models for near wall turbulence. AIAA Journal, 30, 1145-1152(1992).
[16] Settles Gary S, Dodson Li J. Hypersonic shockboundarylayer interaction database[C]22nd Fluid Dynamics, Plasma Dynamics Lasers Conference, 1991: 1763.