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本文引用的文献

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Seedless velocimetry at 100  kHz with picosecond-laser electronic-excitation tagging.采用皮秒激光电子激发标记的100kHz无籽测速技术。
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Selective two-photon absorptive resonance femtosecond-laser electronic-excitation tagging velocimetry.选择性双光子吸收共振飞秒激光电子激发标记测速法
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Femtosecond laser electronic excitation tagging for quantitative velocity imaging in air.用于空气中定量速度成像的飞秒激光电子激发标记
Appl Opt. 2011 Sep 10;50(26):5158-62. doi: 10.1364/AO.50.005158.
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Simultaneous velocity and temperature measurements in gaseous flow fields using the VENOM technique.利用 VENOM 技术同时测量气体流场中的速度和温度。
Opt Lett. 2011 Jan 15;36(2):196-8. doi: 10.1364/OL.36.000196.
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在含有痕量空气的R134a中进行飞秒激光标记。

Femtosecond laser tagging in R134a with trace quantities of air.

作者信息

Zhang Yibin, Danehy Paul M, Miles Richard B

机构信息

Princeton University, Princeton, NJ, 08540.

NASA Langley Research Center, Hampton, VA 23681.

出版信息

AIAA J. 2019 May;57(5):1793-1800. doi: 10.2514/1.J057156. Epub 2019 Jan 11.

DOI:10.2514/1.J057156
PMID:33442067
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7802786/
Abstract

Femtosecond laser tagging is demonstrated for the first time in R134a (1,1,1,2-Tetrafluoroethane) gas, and in mixtures of R134a with small quantities of air. A systematic study of this tagging method is explored through the adjustment of gas pressure, mixture ratio and laser properties. It is found that the signal strength and lifetime are greatest at low pressures for excitation at both the 400 nm and 800 nm laser wavelengths. The relative intensities of two spectral peaks in the near-UV emission change as a function of gas pressure and can potentially be used for local pressure measurements. Single shot precision in pure R134a and R134a with 5% air is demonstrated in quiescent gas and at the exit of a subsonic pipe flow. One standard deviation (68%) of the uncertainty lies within 5 m/s of the mean velocity in a low pressure quiescent flow using a delay time of 3s, and 18 m/s in a 230 m/s flow using a delay of 5 s. The parameter space of these results are chosen to mimic conditions used in the NASA Langley Research Center's Transonic Dynamics Tunnel. The precision and signal lifetime demonstrate the feasibility of using this technique for measuring flowfields that induce airfoil flutter.

摘要

首次在R134a(1,1,1,2 - 四氟乙烷)气体以及R134a与少量空气的混合物中展示了飞秒激光标记。通过调整气体压力、混合比例和激光特性,对这种标记方法进行了系统研究。研究发现,在400nm和800nm激光波长激发时,低压下信号强度和寿命最大。近紫外发射中两个光谱峰的相对强度随气体压力变化,有可能用于局部压力测量。在静态气体以及亚音速管道流出口处,展示了纯R134a和含5%空气的R134a的单次测量精度。在低压静态流中使用3s延迟时间时,不确定度的一个标准偏差(68%)在平均速度的5m/s范围内;在230m/s的流中使用5s延迟时,为18m/s。选择这些结果的参数空间以模拟美国国家航空航天局兰利研究中心跨音速动力学风洞使用的条件。精度和信号寿命证明了使用该技术测量诱导翼型颤振的流场的可行性。