首页> 外文学位 >Investigation of stretch and curvature effects on flames.
【24h】

Investigation of stretch and curvature effects on flames.

机译:研究拉伸和曲率对火焰的影响。

获取原文
获取原文并翻译 | 示例

摘要

Flame response on curvature is very important for understanding and predicting of both laminar and turbulent combustion. In this work, curvature effects on flames are studied analytically, numerically, and experimentally by comparing the opposed jet flame and tubular flame. The cold flow field of the tubular burner and the opposed tubular burner is solved analytically and the appropriate choice of stretch rates is given for comparison of different flames. The analytical solutions are compared to numerical solutions to verify the results. A physical analysis using basic conservation equations to study stretch and curvature effects on premixed flames is carried out. It shows that the curvature effects are coupled with the stretch effects for the first time. The positive curvature strengthens the preferential diffusion and the negative curvature weakens the preferential diffusion; the strengthening or weakening effect is proportional to the ratio of flame thickness to flame radius. Based on the analysis, correlations on flame speed and flame temperature for the stretched and curved flames are given. With these correlations, the flame speed and flame temperature for the curved stretched flames can be predicted from the information of stretched planar flames. The asymptotic analysis for the flame speed and flame temperature of three specific stretched and curved premixed flames: the opposed jet flame, the tubular flame, and the spherical flame is resolved. The comparison between the asymptotic solutions and the numerical solutions is satisfied. With the correlations derived from the physical analysis, the asymptotic solutions can be extended to flame with any values of stretch rate, curvature and Lewis number. The opposed jet and opposed tubular diffusion flames are compared numerically. The curvature influence on diffusion flame temperature and extinction is revealed precisely for the first time. The result shows that the curvature theory on premixed flames can be extended to diffusion flames with excellent results. The curvature affects the diffusion flames by the same mechanism found in premixed flames (i.e. by strengthening or weakening the preferential diffusion). Resulting from the preferential diffusion, curvature has important influence on flame temperature and extinction stretch rate if the Lewis numbers are far away from unity and the ratio of flame thickness to flame radius is on the order of unity. The measured flame properties and flame structure with laser-induced Raman scattering are compared between the opposed jet premixed flame and the tubular premixed flame (Lean H2, CH4 and C3h8 premixed flames). The multicomponent transport model is necessary for good prediction of the lean H2 flames. The experimental results have good agreement with the numerical simulation and are consistent with the theoretical analysis.
机译:曲率上的火焰响应对于理解和预测层流和湍流燃烧都非常重要。在这项工作中,通过比较相对的喷射火焰和管状火焰,对火焰的曲率效应进行了分析,数值和实验研究。通过解析解决了管状燃烧器和相对的管状燃烧器的冷流场,并给出了拉伸速率的适当选择,以比较不同的火焰。将解析解与数值解进行比较以验证结果。进行了使用基本守恒方程的物理分析,以研究拉伸和曲率对预混火焰的影响。它显示了曲率效应与拉伸效应的首次结合。正曲率会增强优先扩散,负曲率会削弱优先扩散。增强或减弱效果与火焰厚度与火焰半径之比成正比。在分析的基础上,给出了拉伸和弯曲火焰的火焰速度和火焰温度的相关性。利用这些相关性,可以从拉伸的平面火焰的信息预测弯曲的拉伸火焰的火焰速度和火焰温度。解析了三种特定的拉伸和弯曲预混火焰的火焰速度和火焰温度的渐近分析:对置射流火焰,管状火焰和球形火焰。满足渐近解与数值解的比较。利用从物理分析得出的相关性,可以将渐近解扩展为具有任意拉伸率,曲率和Lewis值的火焰。数值比较了相对的射流和相对的管状扩散火焰。曲率对扩散火焰温度和消光的影响是首次精确显示。结果表明,预混火焰的曲率理论可以推广到扩散火焰,具有优异的效果。曲率通过在预混火焰中发现的相同机理影响扩散火焰(即通过增强或减弱优先扩散)。由于优先扩散,如果路易斯数远离单位且火焰厚度与火焰半径之比在单位数量级,则曲率对火焰温度和消光拉伸速率具有重要影响。在对置的射流预混火焰与管状预混火焰(稀H2,CH4和C3h8预混火焰)之间比较了测量的火焰特性和具有激光诱导的拉曼散射的火焰结构。多组分传输模型对于良好地预测贫氢火焰是必不可少的。实验结果与数值模拟吻合良好,与理论分析吻合。

著录项

  • 作者

    Wang, Peiyong.;

  • 作者单位

    Vanderbilt University.;

  • 授予单位 Vanderbilt University.;
  • 学科 Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 154 p.
  • 总页数 154
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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