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Computational and experimental study of nonequilibrium chemistry in hypersonic flows.

机译:高超声速流动中非平衡化学的计算和实验研究。

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The accurate prediction of hypersonic flows requires models for thermochemical processes which occur in the flowfield. The gas around a hypersonic vehicle will be hot enough to cause chemical reactions and thermal nonequilibrium. This dissertation is concerned with the coupling between the dissociation rate and the vibrational relaxation process. Because of the large flow speeds, the time scales of the dissociation and vibrational relaxation are the same as the fluid motion time scale. Therefore, the gas will be in thermo-chemical nonequilibrium and these processes must be modeled in coupled manner.; There are many proposed models to account for vibration-dissociation coupling effects, but because of a lack of appropriate experimental data, none of the models have been validated. The purpose of this work is to obtain experimental data from the T5 Shock Tunnel at the California Institute of Technology that can be used to evaluate vibration-dissociation coupling models.; The numerical method and basic thermo-chemical models used were validated by reproducing existing T5 data for blunt body geometries with little vibrational nonequilibrium. Computational fluid dynamics was used to design new experiments. Double-wedge and double-cone geometries were identified as producing flowfields that were very sensitive to vibration-dissociation coupling effects. The mechanism responsible for producing this sensitivity was a shock-wave/boundary-layer interaction that is also present in perfect gas flows. This discovery led to a set of perfect gas double-cone experiments which were used to validate the numerical method for high Mach number flows with large separation zones.; Double-wedge and double-cone models were then tested in T5. Mach-Zehnder interferograms were taken along with surface pressure and heat transfer rate measurements. It was found that computations were unable to reproduce the experimental results, even for flowfields insensitive to vibration-dissociation coupling effects. An analysis of the results showed that the reason for the disagreement is uncertainty in both the equilibrium and nonequilibrium dissociation rates. The double-wedge and double-cone flowfields are a much more sensitive test of the temperature dependence of the dissociation rates than blunt body flowfields, and these results indicate that equilibrium dissociation rates for nitrogen are not as well known as has been believed.
机译:对超音速流的准确预测需要在流场中发生热化学过程的模型。高超音速飞行器周围的气体会变得很热,足以引起化学反应和热不平衡。本文涉及解离速率与振动松弛过程之间的耦合。由于流速大,解离和振动弛豫的时间尺度与流体运动的时间尺度相同。因此,气体将处于热化学非平衡状态,必须以耦合方式对这些过程进行建模。提出了许多模型来解释振动-解离耦合效应,但是由于缺乏适当的实验数据,没有一个模型得到验证。这项工作的目的是从加利福尼亚理工学院的T5冲击隧道获得实验数据,该数据可用于评估振动解离耦合模型。通过复制现有的T5数据以验证几乎没有振动不平衡的钝体几何体,从而验证了所使用的数值方法和基本的热化学模型。计算流体动力学用于设计新实验。双楔形和双锥几何形状被确定为对振动-解离耦合效应非常敏感的产生流场。引起这种敏感性的机制是冲击波/边界层的相互作用,这种相互作用也存在于理想的气流中。这一发现导致了一组完美的气体双锥实验,这些实验被用来验证具有大分离区的高马赫数流的数值方法。然后在T5中测试了双楔形和双锥模型。随表面压力和传热速率的测量结果获取了马赫曾德尔干涉图。发现即使对于对振动-解离耦合效应不敏感的流场,计算也无法重现实验结果。结果分析表明,出现分歧的原因是平衡解离速率和非平衡解离速率均不确定。与钝体流场相比,双楔流和双锥流场对解离速率的温度依赖性测试更为敏感,这些结果表明,人们对氮的平衡解离速率的认识不如人们所认为的那样。

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