Temperature and heat flux measurement technologies in scramjet
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摘要: 测量超燃冲压发动机内部温度及热流场可以为表征、评估、优化其工作状态与性能提供重要支撑。本文综述了可用于发动机温度及热流测量的接触式（铠装及薄膜式）传感器、非接触式（光电及辐射式）测量技术的研究现状及特点。重点介绍了薄膜式热电偶及热流计的发展趋势以及在高温瞬时测量领域的应用前景。最后，对超燃冲压发动机温度及热流测量技术进行了展望。Abstract: The accurate measurement of temperature and heat flux field in scramjet provides strong support for characterization, assessment and optimization of scramjet engine. Measurement methods are reviewed and analyzed, including sheathed and thin film sensors, and photoelectric method and radiation method. Researches of thin film sensors are introduced, and the applications of thin film thermocouple and heat flux sensors in scramjet are pointed out.
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Key words:
- scramjet /
- high-temperature /
- heat flux /
- thin-film thermocouples /
- thin-film heat flux
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图 1 嵌入碳碳复合材料的热电偶安装图
Figure 1. Thermocouples mounted on the backside of the panels using graphite adhesive
图 4 用于分布式壁面温度测量的热电偶及测量结果
Figure 4. Temperature distribution around the cavity flame holder
图 15 基于热图法的Ma=11时超高声速飞行器表面热流分布情况
Figure 15. Averaged heat flux image obtained by using the analytical method from temperature data when Ma=11
图 16 在振荡流场中的壁面热流、流速与温度差对比曲线
Figure 16. Time-resolved data for heat flux vs. flow velocity & temperature difference for a periodically pulsating flow
图 18 Lewis中心研制的薄膜热流计
Figure 18. The heat flux sensors designed by Lewis research center
图 20 Glenn中心研制的薄膜热流计
Figure 20. The heat flux sensors designed by Glenn research center
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