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A variable turbulent Prandtl and Schmidt number model study for scramjet applications.

机译:用于超燃冲压发动机应用的可变湍流Prandtl和Schmidt数模型研究。

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摘要

A turbulence model that allows for the calculation of the variable turbulent Prandtl (Prt) and Schmidt (Sct) numbers as part of the solution is presented. The model also accounts for the interactions between turbulence and chemistry by modeling the corresponding terms. Four equations are added to the baseline k-zeta turbulence model: two equations for enthalpy variance and its dissipation rate to calculate the turbulent diffusivity, and two equations for the concentrations variance and its dissipation rate to calculate the turbulent diffusion coefficient. The underlying turbulence model already accounts for compressibility effects. The variable Prt /Sct turbulence model is validated and tuned by simulating a wide variety of experiments. Included in the experiments are two-dimensional, axisymmetric, and three-dimensional mixing and combustion cases. The combustion cases involved either hydrogen and air, or hydrogen, ethylene, and air.;Two chemical kinetic models are employed for each of these situations. For the hydrogen and air cases, a seven species/seven reaction model where the reaction rates are temperature dependent and a nine species/nineteen reaction model where the reaction rates are dependent on both pressure and temperature are used. For the cases involving ethylene, a 15 species/44 reaction reduced model that is both pressure and temperature dependent is used, along with a 22 species/18 global reaction reduced model that makes use of the quasi-steady-state approximation.;In general, fair to good agreement is indicated for all simulated experiments. The turbulence/chemistry interaction terms are found to have a significant impact on flame location for the two-dimensional combustion case, with excellent experimental agreement when the terms are included. In most cases, the hydrogen chemical mechanisms behave nearly identically, but for one case, the pressure dependent model would not auto-ignite at the same conditions as the experiment and the other chemical model. The model was artificially ignited in that case. For the cases involving ethylene combustion, the chemical model has a profound impact on the flame size, shape, and ignition location. However, without quantitative experimental data, it is difficult to determine which one is more suitable for this particular application.
机译:作为解决方案的一部分,提出了一种湍流模型,该模型允许计算可变湍流的Prandtl(Prt)和Schmidt(Sct)数。该模型还通过对相应项进行建模来说明湍流和化学之间的相互作用。向基线k-zeta湍流模型添加了四个方程式:两个方程式用于计算焓变及其消散率,以计算湍流扩散率;两个方程式用于浓度变化及其消散率,以计算湍流扩散系数。潜在的湍流模型已经考虑了可压缩性的影响。通过模拟各种实验来验证和调整可变的Prt / Sct湍流模型。实验中包括二维,轴对称和三维混合和燃烧情况。燃烧案例涉及氢气和空气,或氢气,乙烯和空气。;对于每种情况,都使用两个化学动力学模型。对于氢气和空气情况,使用反应速率与温度有关的七种/七种反应模型和反应速率取决于压力和温度的九种/十九种反应模型。对于涉及乙烯的情况,使用了15种/ 44依赖于压力和温度的反应减少模型,以及22种/ 18的利用准稳态近似的全局反应减少模型。 ,表明所有模拟实验的一致性都很好。发现在二维燃烧情况下,湍流/化学相互作用项对火焰位置有重大影响,当包括这些项时,具有极好的实验一致性。在大多数情况下,氢化学机理的行为几乎相同,但是对于一种情况,压力相关模型在与实验和另一化学模型相同的条件下不会自动点火。在这种情况下,该模型是人为点燃的。对于涉及乙烯燃烧的情况,化学模型对火焰的大小,形状和点火位置有深远的影响。但是,如果没有定量的实验数据,很难确定哪一种更适合这种特定应用。

著录项

  • 作者

    Keistler, Patrick.;

  • 作者单位

    North Carolina State University.;

  • 授予单位 North Carolina State University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 156 p.
  • 总页数 156
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:38:12

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