Thermal-optical Analysis for Optical Window under High Mach Flight condition
When the airborne platform, where installed the optical window, is in high Mach flight condition. The aerodynamic heating effect, which will influence optical properties of optical window, becomes very obvious. This special flight condition will change shape, refractive index and also refractive index distribution of optical window due to the generated high axial temperature gradient. To ensure image quality of aerial remote sensor, the present paper does thermal-optical analysis for optical window under high Mach flight condition. Then, on this basis, do simulations according to theoretical analysis and boundary conditions derived from practical assumptions in order to get the final conclusions.
aerial remote sensor optical window high Mach flight condition refractive index refractive index distribution
Chongliang Zhong Yalin Ding Jinbao Fu
Key Laboratory of Airborne Optical Imaging andMeasurement, Changchun institute of Optics, FineMechan Key Laboratory of Airborne Optical Imaging and Measurement, Changchun institute of Optics, Fine Mech University of Chinese Academy of SciencesBeijing, China Changchun institute of Optics, Fine Mechanic
国际会议
2012 International Conference on Optoelectronics and Microelectronics(2012光电子与微电子国际学术会议 2012 ICOM)
长春
英文
319-322
2012-08-23(万方平台首次上网日期,不代表论文的发表时间)