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Probing the Vibrational Relaxation of N2 and O2 by Use of CARS Spectroscopy to Model NTE-Turbulence

机译:利用CARS光谱法对NTE和湍流进行模拟以探测N2和O2的振动弛豫

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摘要

The thermochemical dynamics associated with hypersonic flight and turbulent flow is vital to understanding the effects that hypersonic turbulence has on objects or vehicles traveling at speeds above Mach 5 (~ 1708 m/s). Non-thermochemical equilibrium (NTE) exists downstream of strong shock fronts and encountered in the shear layers from hypersonic flight, and coupled with turbulence, it has significant effects on flow dynamics. NTE, characterized by high vibrational temperatures of N2 and O2, was observed, and the relaxation processes were measured to obtain time-resolved results. By inducing cold-flow NTE via RF-plasma, species in the flow were probed to determine specific vibrational temperatures at particular distances and times following initial NTE-preparation. The detection technique used in the experiment was coherent anti-Stokes Raman spectroscopy (CARS) and variations of this laser-based technique were optimized to maximize accuracy and signal-to-noise in the vibrational relaxation measurements. It was found that the boxCARS variant was most successful in probing the v=1 --> v=0 vibrational transition associated with the measurement. Also a dual pump-beam CARS setup enabled the probing of both N2 and O2 simultaneously; however, in this report only N2 vibrational relaxation was modeled because the lifetime of vibrationally-excited (v=1) O2 was too short and the O2 vibrational temperature was too low to model. The CARS spectra were obtained in a subsonic wind tunnel with a flow velocity of approximately 30 m/s and probing distances from 4.4-39.4 cm downstream the plasma. Five averaged vibrational temperature values were determined and they yielded a decay from 1882 ? 46 K (4.4 cm from plasma) to 1010 ? 16 K (39.4 cm from plasma) showing the relative rate of vibrational relaxation of N2. The vibrational relaxation was also modeled as a function of time after passing through the plasma, and a kinetic simulation was fit to the results. The spectral decay of the v=1 peak relative to v=0 (Iv=1/Iv=0) was found and compared to the decay of the vibrational temperature. Data analysis revealed that the results were in agreement with theory and the observed vibrational relaxation of N2 fit the simulated kinetic model accurately.
机译:高超声速飞行和湍流相关的热化学动力学对于理解高超声速湍流对以高于5马赫(〜1708 m / s)的速度行驶的物体或车辆的影响至关重要。非热化学平衡(NTE)存在于强冲击波前沿的下游,并在高超声速飞行的剪切层中遇到,并且加上湍流,它对流动动力学有重要影响。观察到以N2和O2的高振动温度为特征的NTE,并测量了弛豫过程以获得时间分辨结果。通过经由RF-等离子体诱导冷流NTE,探测流中的物质,以确定在初始NTE制备后特定距离和时间的特定振动温度。实验中使用的检测技术是相干反斯托克斯拉曼光谱(CARS),并且优化了此基于激光的技术的变化形式,以最大程度地提高振动弛豫测量的准确性和信噪比。发现boxCARS变体在探测与测量相关的v = 1-> v = 0振动跃迁方面最成功。同样,双泵束CARS设置可以同时探测N2和O2。但是,在此报告中,仅模拟了N2振动弛豫,因为振动激发的(v = 1)O2的寿命太短,并且O2振动温度太低而无法建模。 CARS光谱是在亚音速风洞中获得的,流速约为30 m / s,在等离子体下游的探测距离为4.4-39.4 cm。确定了五个平均振动温度值,它们从1882年开始衰减。 46 K(距血浆4.4厘米)至1010? 16 K(距离等离子体39.4 cm)显示N2振动弛豫的相对速率。振动弛豫也被建模为通过等离子体后的时间函数,并且动力学模拟符合结果。发现相对于v = 0(v = 1 / Iv = 0)的v = 1峰的频谱衰减,并将其与振动温度的衰减进行比较。数据分析表明,该结果与理论相符,并且观察到的N2的振动弛豫准确地拟合了模拟的动力学模型。

著录项

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    Dean Jacob;

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  • 年度 2009
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  • 原文格式 PDF
  • 正文语种 en_US
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