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高超声速热线/热膜风速仪研究综述及分析

韦青燕 张天宏

测试技术学报2012,Vol.26Issue(2):142-149,8.
测试技术学报2012,Vol.26Issue(2):142-149,8.DOI:10.3969/j.issn.1671-7449.2012.02.010

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

韦青燕 1张天宏1

作者信息

  • 1. 南京航空航天大学能源与动力学院,江苏南京210016
  • 折叠

摘要

Abstract

In terms of the requirements for hot - wire/film anemometry in hypersonic airflow measurement, the recent research and development of hot - wire/film anemometry are summarized. The key problems and technical features are discussed for hypersonic hot-wire/film anemometry based on probe manufacture, control circuit design and probe calibration. The effects on thermal testing system are analyzed form hot-wire/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

Key words

hypersonic/ hot-wire/film probe/ anemometry control-circuit model/ calibration method

分类

信息技术与安全科学

引用本文复制引用

韦青燕,张天宏..高超声速热线/热膜风速仪研究综述及分析[J].测试技术学报,2012,26(2):142-149,8.

基金项目

国家自然科学基金资助项目(51176075) (51176075)

测试技术学报

OACSTPCD

1671-7449

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