红外技术, 2017, 39 (8): 746, 网络出版: 2017-10-30
临近空间高超声速飞行器红外特性建模仿真
Infrared Simulation of Near Space Hypersonic Vehicle
临近空间 高超声速飞行器 红外仿真 红外特性 near space hypersonic vehicle infrared simulation infrared radiation characteristics
摘要
本文针对临近空间高超声速飞行器的红外特性进行建模仿真与分析。以美国X-51A 的飞行器模型为例， 综合考虑目标的运动状态、大气环境等的影响作用， 使用FLUENT 软件和SE-WORKBENCH-EO 软件建立目标三维温度场模型和红外特性模型，并分析其红外特性。
Abstract
In this paper, research on infrared simulation of a near space hypersonic vehicle is presented. Considering X-51A as an example, the model for calculation of the 3D temperature and infrared flux of the target was developed using FLUENT and SE-WORKBENCH-EO, with comprehensive consideration of external influences, such as the impact of the atmospheric environment, the movement of the target, etc. The infrared characteristics of the target have been analyzed.
周方方, 张二磊, 陈宜峰. 临近空间高超声速飞行器红外特性建模仿真[J]. 红外技术, 2017, 39(8): 746. ZHOU Fangfang, ZHANG Erlei, CHEN Yifeng. Infrared Simulation of Near Space Hypersonic Vehicle[J]. Infrared Technology, 2017, 39(8): 746.
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