REMPI刺激下氮羽流的流速测量

C. Dankert, H. Mori
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引用次数: 0

摘要

在dlr -高真空羽流试验装置STG上,以N/ sub2 /为试验气体,进行了超声速羽流向真空膨胀的实验研究。测量值为皮托管压力、分子数通量、旋转温度和密度。后两个量通过2+2 REMPI技术测量,激发波长为283 ~ 284 nm (REMPI =共振增强多光子电离)。该方法也适用于离子飞行时间(TOF)法测量绝对流速。结合REMPI和TOF技术的装置类似于使用电子束轰击的TOF实验,但使用聚焦激光束代替电子束。这种激光测量的结果在高度稀薄的羽流在几个停滞温度给出了氮气作为测试气体。轴向计算结果与理论极限速度完全吻合;讨论了离轴角速度分布,并与理论进行了比较。本文研究了从超声速喷嘴向真空膨胀的稀薄羽流中N/sub - 2/的流动速度的实验方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flow velocity measurements in nitrogen plumes stimulated by REMPI
In the DLR-high vacuum plume test facility STG, experiments have been performed to study the expansion of supersonic plumes into vacuum with N/sub 2/ as a test gas. The measured values were the Pitot pressure, the molecular number flux, the rotational temperature and the density. The last two quantities were measured by the 2+2 REMPI-technique with a stimulation wavelength of 283-284 nm (REMPI = resonance enhanced multi photon ionization). This method is also suitable to measure the absolute flow velocity by the ion time-of-flight (TOF) method. The apparatus for the combination of the REMPI and TOF technique is similar to that for the TOF experiments using electron beam bombardment, but a focused laser beam is used instead of an electron beam. The results of such laser measurements in highly rarefied plumes for several stagnation temperatures are presented with nitrogen as test gas. On-axis results fit well with the theoretical limiting velocity for perfect expansion; angular velocity profiles off-axis are discussed and compared to theory. This study is focused on the experimental procedure to measure the flow velocity of N/sub 2/ in rarefied plumes expanding from supersonic nozzles into vacuum.
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