A calculation approach for shock layer radiation and transmittance towards hypersonic infrared homing vehicle
Pang MQ(庞明琪)1,2,3,4; Shi ZL(史泽林)1,2,3,4; Zhang DJ(张代军)1,3,4; Liu HZ(刘海峥)1,3,4
2021
会议日期June 20-22, 2021
会议地点Beijing, China
关键词hypersonic shock layer radiation transmissivity
页码1-6
英文摘要In order to study the optical transmission and radiation characteristics in a hypersonic shock layers over infrared optical window, an approximation calculation approach is proposed. With this method, the formal solution for shock layer radiative transport equation is derived considering both target signature and windows thermal radiance. Consequently, the transmissivity of heating shock layer can be expressed quantitatively, which shows that the shock layer is optically thick in the 4∼4.5μm band mainly. Besides, the radiance flux density of shock layer is calculated when temperature is 800K, pressure is 7atm and thickness is 1cm. Shock layer radiance is found to be larger in the mid-wave infrared band compared with long-wave infrared band and short-wave infrared band.
产权排序1
会议录2021 Applied Optics and Photonics China: Infrared Device and Infrared Technology, AOPC 2021
会议录出版者SPIE
会议录出版地Bellingham, USA
语种英语
ISSN号0277-786X
ISBN号978-1-5106-4997-2
WOS记录号WOS:000767060000044
内容类型会议论文
源URL[http://ir.sia.cn/handle/173321/30278]  
专题沈阳自动化研究所_光电信息技术研究室
通讯作者Pang MQ(庞明琪)
作者单位1.Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110169, China
2.Department of Automation, University of Science and Technology of China, Hefei 230027, China
3.Key Laboratory of Optical-Electronics Information Processing, Chinese Academy of Sciences, Shenyang 110016, China
4.Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China
推荐引用方式
GB/T 7714
Pang MQ,Shi ZL,Zhang DJ,et al. A calculation approach for shock layer radiation and transmittance towards hypersonic infrared homing vehicle[C]. 见:. Beijing, China. June 20-22, 2021.
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