Infrared and Laser Engineering, Volume. 49, Issue 4, 0404002(2020)
Radiative transmission property of infrared window in hypersonic vehicle
[4] [4] Cross E F. Windowheating effects on airbne infrared system calibration [C]Proceedings of SPIE, 1992, 1762: 576−583.
[6] 王亚辉, Yahui Wang, 王强, Qiang Wang, 张伯川, Bochuan Zhang. Evaluation method for aero-thermo-radiation effect of IR window. Infrared and Laser Engineering, 45, 0404002(2016).
[7] 王惠, Hui Wang, 党凡阳, Fanyang Dang, 张荣达, Rongda Zhang. Influence of thickness of hemispherical dome on aerodynamic thermal radiation. Infrared and Laser Engineering, 47, 153-158(2018).
[8] [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] [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] [10] Zhang S, Fang C, Hong L. Integrated fluidthermalstructural analysis f predicting aerothermal environment of hypersonic vehicles[C]Aerospace Sciences Meeting, 2013.
[12] [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] [16] Settles Gary S, Dodson Li J. Hypersonic shockboundarylayer interaction database[C]22nd Fluid Dynamics, Plasma Dynamics Lasers Conference, 1991: 1763.
Get Citation
Copy Citation Text
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
The Author Email: