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高超声速钝锥模型及其尾迹红外辐射实验研究
Experimental research on infrared radiation from hypersonic blunt cone and wake
【摘要】 介绍了利用InSb红外辐射计在弹道靶上测量底部直径为10mm、半锥角和头部半径分别为9°、2.2mm(模型A),8°、0.6mm(模型B)的两种非烧蚀钝锥模型及其尾迹的红外辐射。模型速度大于6km/s,飞行环境压力约4.8kPa,红外辐射测量波段为1~3μm、3~5μm。结果表明:非烧蚀钝锥模型头身部红外辐射远大于尾迹红外辐射,在相同飞行速度和环境压力条件下,模型A产生的红外辐射比模型B产生的红外辐射强。
【Abstract】 The experiment of measuring infrared radiation of non-ablation blunt cone and wake using InSb infrared radiometers on ballistic range is described in this paper.The IR radiation distributions in 1~3μm and 3~5μm bands for model A with 10mm base diameter,9° half-cone angle,2.2mm head radius and model B with 10mm base diameter,8° half-cone angle,0.6mm head radius are obtained.The model velocity is over 6km/s,and environment pressure is about 4.8kPa.The results show that the IR radiation of model is stronger than the IR radiation of wake,and the IR radiation of model A is stronger than model B at the same test conditions.
- 【文献出处】 实验流体力学 ,Journal of Experiments in Fluid Mechanics , 编辑部邮箱 ,2006年02期
- 【分类号】V216
- 【被引频次】2
- 【下载频次】152