Research progress and thinking of infrared aero-optical effect (Invited)

被引:1
|
作者
Xing Z. [1 ]
Chen X. [1 ]
Peng Z. [1 ]
Yang Z. [2 ]
Zhang H. [1 ]
Xing Z. [1 ]
Zhang N. [3 ]
机构
[1] Tianjin Jinhang Institute of Technical Physics, Tianjin
[2] The Third Military Representative Office in Tianjin of Military Representative Agency in Beijing of the Air Force Equipment Department, Tianjin
[3] Beijing Electro-mechanical Engineering Institute, Beijing
关键词
Aero-optics; Image correction; Infrared detection; Numerical simulation; Wind tunnel;
D O I
10.3788/IRLA20220228
中图分类号
学科分类号
摘要
Infrared imaging detection technology is an important means of precision guidance. With the development of missile weapons to supersonic and hypersonic, the working environment of infrared imaging detection devices is worse. The structure safety of infrared windows faces great challenges because of the severe aerodynamic thermal environment in high speed flight. The radiation interference of high-temperature radiation sources such as shock wave and window seriously affects the infrared detection ability. The transmission effect of flow field and window reduces the detection and guidance accuracy. Aero-optical effect is the most essential difference between high-speed infrared detection and traditional infrared detection, and it is also the key factor to determine the feasibility of infrared detection applied to high-speed missiles. This paper mainly introduced the aerodynamic thermal effect, thermal radiation effect, transmission effect and their influence of high-speed infrared imaging detection, expounded the progress of aero-optical effect in mechanism research, test research, numerical simulation and correction technology, and finally gave the thoughts and suggestions on the research of aero-optical effect of high-speed infrared detection. Copyright ©2022 Infrared and Laser Engineering. All rights reserved.
引用
收藏
相关论文
共 113 条
  • [31] Song Minmin, Wang Biyun, Wang Shuang, Et al., Thermal radiation calculation of optical dome for high speed vehicl, Aerospace Shanghai, 33, 4, pp. 50-55, (2016)
  • [32] Xue Wenhui, Research on the thermal radiation characteristics of conformal dome in the aero-dynamic environment, (2016)
  • [33] Wang Jian, The thermal radiation building and emulation of optical dome in aerodynamic thermal environment, (2010)
  • [34] Gao Xilei, Modeling and simulation of the aerodynamic heating of dome influence on the imaging system, (2013)
  • [35] Cheng Meisha, Chen Lianzhong, Aero-optics testing schemes for infrared radome, Aerospace Materials & Technology, 40, 3, pp. 73-75, (2010)
  • [36] Chen Lianzhong, Zhang Jiaxiang, Fei Jindong, Experiment research on the aerodynamic heating effect on the infrared imaging, Laser & Infrared, 39, 1, pp. 36-38, (2009)
  • [37] Yin Xingliang, Aero-Optical Principle [M], (2003)
  • [38] Liu Yuanchun, Yuan Ziguan, He Yurong, Et al., Numerical simulation of jammer saturation of thermal radiation effect on two-dimensional optical domes, Journal of Harbin Engineering University, 36, 10, pp. 1356-1360, (2015)
  • [39] Liu Yuanchun, Hua Zhiwei, He Yurong, Et al., Investigation of thermal radiation effect on optical dome of sapphire coated yttrium oxide, Science Bulletin, 61, 10, pp. 801-810, (2016)
  • [40] Wang Hui, Dang Fanyang, Zhang Rongda, Et al., Influence of thickness of hemispherical dome on aerodynamic thermal radiation, Infrared and Laser Engineering, 47, 12, (2018)