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Experimental and Computational Analyses of Methane and Hydrogen Mixing in a Model Premixer

机译:模型预混合器中甲烷和氢气混合的实验和计算分析

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摘要

The mixing of fuel and air in combustion systems plays a key role in overall operability and emissions performance. Such systems are also being looked to for operation on a wide array of potential fuel types, including those derived from renewable sources such as biomass or agricultural waste. The optimization of premixers for such systems is greatly enhanced if efficient design tools can be utilized. The increased capability of computational systems has allowed tools such as computational fluid dynamics to be regularly used for such purpose. However, to be applied with confidence, validation is required. In the present work, a systematic evaluation of fuel mixing in a specific geometry, which entails cross flow fuel injection into axial nonswirling air streams has been carried out for methane and hydrogen. Fuel concentration is measured at different planes downstream of the point of injection. In parallel, different computational fluid dynamics approaches are used to predict the concentration fields resulting from the mixing of fuel and air. Different steady turbulence models including variants of Reynolds averaged Navier-Stokes (RANS) have been applied. In addition, unsteady RANS and large eddy simulation are used. To accomplish mass transport with any of the RANS approaches, the concept of the turbulent Schmidt number is generally used. As a result, the sensitivity of the RANS simulations to different turbulent Schmidt number values is also examined. In general, the results show that the Reynolds stress model, with use of an appropriate turbulent Schmidt number for the fuel used, provides the best agreement with the measured values of the variation in fuel distribution over a given plane in a relatively time efficient manner. It is also found that, for a fixed momentum flux ratio, both hydrogen and methane penetrate and disperse in a similar manner for the flow field studied despite their significant differences in density and diffusivity.
机译:燃烧系统中燃料和空气的混合在总体可操作性和排放性能中起着关键作用。人们还希望此类系统能够在多种潜在燃料类型上运行,包括从可再生资源(如生物质或农业废弃物)中获得的燃料。如果可以使用有效的设计工具,则可以大大增强此类系统的预混器优化。计算系统能力的提高使得诸如计算流体动力学之类的工具可以定期用于此目的。但是,要放心使用,必须进行验证。在当前的工作中,已经对甲烷和氢气中特定几何形状的燃料混合进行了系统评估,这需要将错流燃料喷射到轴向非旋流空气中。在喷射点下游的不同平面上测量燃油浓度。并行地,使用不同的计算流体动力学方法来预测由燃料和空气的混合产生的浓度场。已应用了不同的稳态湍流模型,包括雷诺平均Navier-Stokes(RANS)的变体。另外,使用了不稳定的RANS和大涡模拟。为了通过任何一种RANS方法完成大规模运输,通常使用湍流Schmidt数的概念。结果,还检查了RANS模拟对不同湍流Schmidt数值的敏感性。总的来说,结果表明,雷诺应力模型在为所使用的燃料使用适当的湍流施密特数的情况下,以相对省时的方式与给定平面上的燃料分布变化的测量值提供了最佳一致性。还发现,对于固定的动量通量比,尽管研究的流场在密度和扩散率上存在显着差异,但氢和甲烷都以相似的方式渗透和扩散。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2011年第10期|p.101503.1-101503.11|共11页
  • 作者单位

    UCI Combustion Laboratory,University of California,Irvine, CA 92697-3550;

    UCI Combustion Laboratory,University of California,Irvine, CA 92697-3550;

    UCI Combustion Laboratory,University of California,Irvine, CA 92697-3550;

    UCI Combustion Laboratory,University of California,Irvine, CA 92697-3550;

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