高超声速热线/热膜风速仪研究综述及分析  

Review and Analysis of Hot-wire/film Anemometry for Hypersonic Airflow Measurement

作　　者：韦青燕[1] 张天宏[1] 

机构地区：[1]南京航空航天大学能源与动力学院,江苏南京210016

出　　处：《测试技术学报》2012年第2期142-149,共8页Journal of Test and Measurement Technology

基　　金：国家自然科学基金资助项目(51176075)

摘　　要：针对高超声速流场测量对热线/热膜风速仪的需求,对近年来国内外热线/热膜风速仪研制现状进行了归纳.重点从探头制备、控制电路设计及探头校准三个方面,阐述了热线/热膜测试系统应用于高超声速流场测量必须解决的关键问题及各种方案的特点;分析了探头材料、构型及控制电路模式对高超声速流场中热线/热膜测试系统性能的影响,并对热线/热膜探头校准的几种方法进行了对比,总结出可供发展我国自主知识产权高超声速热线/热膜技术的意见.In terms of the requirements for hotwire/film anemometry in hypersonic airflow measurement, the recent research and development of hotwire/film anemometry are summarized. The key problems and technical features are discussed for hypersonic hotwire/film anemometry based on probe manufacture, control circuit design and probe calibration. The effects on thermal testing system are analyzed form hotwire/film material, geometry and control circuit mode, and several calibration methods are compared. Finally, some approaches have been proposed as reference to the research of hypersonic anemometry in China.

关 键 词：高超声速 热线/热膜探头 风速仪控制电路模式 校准方法 

分 类 号：TP212[自动化与计算机技术—检测技术与自动化装置]