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Thermal-optical evaluation to optical window of near space aerial remote sensor surrounding hypersonic
Zhang H.; Cao G.; Li Y.; Zhang J.
2014
发表期刊Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering
ISSNISBN/10072276
卷号43期号:12页码:3958-3962
摘要In order to improve the optical performance of optical window in aerial remote sensor, thermal-optical evaluation to fused silica optical window surrounding hypersonic was analyzed. The flight environment of optical window was analyzed. Based on the theory of aerodynamics, the relation between convection heat transfer coefficient and mach number was calculated. The temperature distributing of optical window was simulated by heat flux density, the optical path difference caused by the temperature difference between the inner and outer surfaces was calculated, and the influence of thermal deformation of the optical window on optical transfer function was analyzed. The study result shows that the optical path difference caused by thermal deformation of the optical window is 130.5 nm, which is under 1/4. The simulation result meets the requirements of the optical design. The above result discussed in this paper can be used as a reference for other optical window designs.
收录类别EI
语种中文
文献类型期刊论文
条目标识符http://ir.ciomp.ac.cn/handle/181722/44471
专题中科院长春光机所知识产出
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Zhang H.,Cao G.,Li Y.,et al. Thermal-optical evaluation to optical window of near space aerial remote sensor surrounding hypersonic[J]. Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering,2014,43(12):3958-3962.
APA Zhang H.,Cao G.,Li Y.,&Zhang J..(2014).Thermal-optical evaluation to optical window of near space aerial remote sensor surrounding hypersonic.Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering,43(12),3958-3962.
MLA Zhang H.,et al."Thermal-optical evaluation to optical window of near space aerial remote sensor surrounding hypersonic".Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering 43.12(2014):3958-3962.
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