On two-dimensional numerical modeling of the Burrows - Kurkov experimental data on hydrogen combustion in a supersonic air flow usingNS/RANS equations

Sergey T. Surzhikov
{"title":"On two-dimensional numerical modeling of the Burrows - Kurkov experimental data on hydrogen combustion in a supersonic air flow usingNS/RANS equations","authors":"Sergey T. Surzhikov","doi":"10.33257/phchgd.22.4.957","DOIUrl":null,"url":null,"abstract":"Using the two-dimensional computer code NERAT-2D, a computational analysis of experimental data on the ignition of a hydrogen jet in a concurrent flow of moist air has been performed. For a numerical study, experimental data were selected [Burrows M.C., Kurkov A.P.] An analytical and experimental study of supersonic combustion of hydrogen in the vitiated air stream. AIAA J. 1973. No.11. Pp. 1217–1218], which have been used for several decades to validate computer codes and physicochemical models of hydrogen combustion in air. Used computer code NERAT-2D implements the numerical integration of two-dimensional Na-vier − Stokes equations on structured multi-block grids. The problem is solved on a sequence of calculation grids without and using Reynolds averaging. The 8-reaction kinetic Evans − Schexnayder model of combustion of molecular hydrogen in hot humid air was used. It is shown that on relatively coarse computational grids, the calculated limit of ignition of a hydrogen jet in an airflow significantly exceeds that measured in the experiment. On detailed computational grids, an unsteady motion of an ignitable hydrogen jet is observed, and the ignition boundary corresponds with good accuracy to the experimental one. As an appendix to the article, a number of animation files are presented that illustrate the unsteady combustion of a hydrogen jet in a co-currents flow of moist air.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"133 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Physical-Chemical Kinetics in Gas Dynamics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.33257/phchgd.22.4.957","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Using the two-dimensional computer code NERAT-2D, a computational analysis of experimental data on the ignition of a hydrogen jet in a concurrent flow of moist air has been performed. For a numerical study, experimental data were selected [Burrows M.C., Kurkov A.P.] An analytical and experimental study of supersonic combustion of hydrogen in the vitiated air stream. AIAA J. 1973. No.11. Pp. 1217–1218], which have been used for several decades to validate computer codes and physicochemical models of hydrogen combustion in air. Used computer code NERAT-2D implements the numerical integration of two-dimensional Na-vier − Stokes equations on structured multi-block grids. The problem is solved on a sequence of calculation grids without and using Reynolds averaging. The 8-reaction kinetic Evans − Schexnayder model of combustion of molecular hydrogen in hot humid air was used. It is shown that on relatively coarse computational grids, the calculated limit of ignition of a hydrogen jet in an airflow significantly exceeds that measured in the experiment. On detailed computational grids, an unsteady motion of an ignitable hydrogen jet is observed, and the ignition boundary corresponds with good accuracy to the experimental one. As an appendix to the article, a number of animation files are presented that illustrate the unsteady combustion of a hydrogen jet in a co-currents flow of moist air.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
利用ns /RANS方程对超声速气流中氢气燃烧的Burrows - Kurkov实验数据进行二维数值模拟
利用NERAT-2D二维计算机代码,对湿空气同步流动中氢气射流点火的实验数据进行了计算分析。数值研究选择了实验数据[Burrows M.C, Kurkov A.P.]变质气流中氢气超声速燃烧的分析与实验研究。Aiaa j . 1973。11路。[p. 1217-1218],几十年来一直用于验证计算机代码和氢在空气中燃烧的物理化学模型。使用计算机代码NERAT-2D在结构化多块网格上实现二维Na-vier - Stokes方程的数值积分。在不使用和使用雷诺平均的情况下,在一系列计算网格上解决了这个问题。采用了分子氢在湿热空气中燃烧的8反应动力学Evans - Schexnayder模型。结果表明,在较粗的计算网格上,计算得到的氢气射流在气流中的点火极限明显超过实验测量值。在详细的计算网格上观测了可燃氢射流的非定常运动,得到的点火边界与实验边界吻合较好。作为文章的附录,我们提供了一些动画文件来说明氢射流在湿空气共流中的不稳定燃烧。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Drag and heat transfer of metal and oxide agglomerates in flow of combustion products of solid propellant On the Possibility of Reducing Friction due to Relaminarization of the Flow in the Pipe Ballistic opportunities' evaluation of artillery projectile with a rocket ramjet Role of giant dielectric permittivity effect during tornado generation process Brittle Cylinder Transfering by a Manipulator with Three Fingers
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1