
第 42 卷 第 7 期
2015 年 7 月
Vol. 42, No. 7
July, 2015
中 国 激 光
CHINESE JOURNAL OF LASERS
0715001-
波长调制-TDLAS 技术测量风洞中氧气流速方法研究
贾良权
1,2
刘文清
1
阚瑞峰
1
刘建国
1*
姚 路
1,2
许振宇
1
戴云海
1
魏 敏
1,3
1
中国科学院安徽光学精密机械研究所环境光学与技术重点实验室, 安徽 合肥 230031
2
中国科学院大学, 北京 100049
3
中国科学技术大学, 安徽 合肥 230031
摘要 为了有效地测量风洞中的气体流速,以激光多普勒频移原理为基础,结合波长调制可调谐二极管激光吸收光谱
(TDLAS)技术,利用 HITRAN 数据库,选取氧气(O
2
)分子在 13144.5 cm
-1
附近的吸收谱线作为研究对象。在软件中建立
了气体流速测量模型,模拟分析了流速测量结果;在实验室中利用超声风洞装置,建立了一套基于波长调制-TDLAS
技术的流速测量系统,通过实验,提取出 O
2
的二次谐波信号,根据 O
2
分子吸收谱线的二次谐波信号的频移量反演风洞
中的气流速度。实验结果表明,在实验室环境下,系统测量流速达到 707.6 m/s,符合超声风洞的设计,测量误差范围
为 5.47%。实验结果为基于波长调制-TDLAS 方法测量流速的小型化系统研制以及飞行实验进行了前期准备。
关键词 光谱学; 流速测量; 可调谐二极管激光吸收光谱; 波长调制; 多普勒频移; 风洞
中图分类号 O346 文献标识码 A
doi: 10.3788/CJL201542.0715001
Study on Oxygen Velocity Measurement in Wind Tunnel by
Wavelength Modulation - TDLAS Technology
Jia Liangquan
1,2
Liu Wenqing
1
Kan Ruifeng
1
Liu Jianguo
1
Yao Lu
1,2
Xu Zhenyu
1
Dai Yunhai
1
Wei Min
1,3
1
Key Laboratory of Environmental Optics and Technology, Anhui Institute of Optics and Fine Mechanics,
Chinese Academy of Sciences, Hefei, Anhui 230031, China
2
University of Chinese Academy of Sciences, Beijing 100049, China
3
University of Science and Technology of China, Hefei, Anhui 230031, China
Abstract In order to effectively measure gas flow rate in wind tunnel, based on the principle of laser Doppler
frequency shift, combined with wavelength modulation tunable diode laser absorption spectroscopy (TDLAS)
technology, using HITRAN database, oxygen (O
2
) molecular absorption spectral line near 13144.5 cm
-1
is selected
as the research object. A gas flow measurement model is built in the software, the flow velocity measurement results
are simulated and analyzed. Supersonic wind tunnel devices are used in the laboratory to set up a set of wavelength
modulation flow measurement system based on TDLAS technology. Through the experiment, second harmonic
signal of O
2
is extracted. According to the second harmonic of O
2
molecular absorption spectral line frequency shift,
the flow velocity in the wind tunnel is reversed. The experimental results show that, in the laboratory environment,
velocity measured by the system reaches 707.6 m/s. The experimental results are consistent with the supersonic
wind tunnel design, and the measurement error is 5.47% . The results prepare for the research of system
miniaturization, which measures flow rate based on wavelength modulation - TDLAS, and flight experiments.
收稿日期: 2014-12-29; 收到修改稿日期: 2015-02-03
基金项目: 国家自然科学基金(61108034)、国家自然科学基金青年基金(61205151)、中国科学院先导专项(XDA05040102)
作者简介: 贾良权(1984—),男,博士研究生,主要从事波长调制 TDLAS 质量流量测量方法方面的研究。
E-mail: lqjia@aiofm.ac.cn
导师简介: 刘文清(1954—),男,中国工程院院士,博士生导师,主要从事环境监测技术方面的研究。
E-mail: wqliu@aiofm.ac.cn
*通信联系人。E-mail: jgliu@aiofm.ac.cn
1