首页> 外文期刊>International journal of hydrogen energy >Large eddy simulation of hydrogen combustion in supersonic flows using an Eulerian stochastic fields method
【24h】

Large eddy simulation of hydrogen combustion in supersonic flows using an Eulerian stochastic fields method

机译:使用欧拉随机场方法对超音速流中氢燃烧的大涡模拟

获取原文
获取原文并翻译 | 示例
       

摘要

An Eulerian Monte-Carlo approach, the so-called Eulerian stochastic fields (ESF) method is implemented and evaluated for simulation of non-premixed hydrogen/air combustion in supersonic flows. The ESF method is integrated into a compressible flow large eddy simulation (LES) solver, and validated on a supersonic combustor with a strut as flame holder. Comparison with experimental data and with results from a well-stirred reactor (WSR) model demonstrates the advantage of the LES-ESF method for simulation of local extinction and re-ignition phenomena. The hydrogen/air flame structure and the stabilization of the combustion process in the supersonic combustor are analysed based on the present LES-ESF method. Oscillation of the recirculation zones is found to be the dominant mechanism for the local-extinction/re-ignition and the flame stabilization under the present condition. (C) 2016 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
机译:实施了欧拉蒙特卡洛方法,即所谓的欧拉随机场(ESF)方法,并进行了评估,以模拟超音速流中未预混合的氢/空气燃烧。 ESF方法已集成到可压缩流大涡模拟(LES)求解器中,并在带有支柱作为火焰保持器的超音速燃烧器上进行了验证。与实验数据和搅拌良好的反应堆(WSR)模型的结果进行比较,证明了LES-ESF方法在模拟局部熄灭和重燃现象方面的优势。基于目前的LES-ESF方法,分析了氢/空气火焰结构以及超音速燃烧室燃烧过程的稳定性。在当前条件下,发现回流区的振荡是局部熄灭/重燃和火焰稳定的主要机制。 (C)2016氢能出版物有限公司。由Elsevier Ltd.出版。保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号