首页> 外文期刊>Combustion Science and Technology >THE INITIAL TEMPERATURE AND N_2 DILUTION EFFECT ON THE LAMINAR FLAME SPEED OF PROPANE/AIR
【24h】

THE INITIAL TEMPERATURE AND N_2 DILUTION EFFECT ON THE LAMINAR FLAME SPEED OF PROPANE/AIR

机译:丙烷/空气层流火焰速度的初始温度和N_2稀释效应

获取原文
获取原文并翻译 | 示例
       

摘要

Laminar flame speeds of propane/air mixtures were determined experimentally over an extensive range of equivalence ratios at room temperature, 500 K, 650 K, and atmospheric pressure. Nitrogen addition to simulate effects of exhaust gas dilution on the laminar flame speed was also studied at these conditions for selected equivalence ratios. The experiments employed the stagnation jet-wall flame configuration in which the flow velocity was obtained by using particle image velocimetry. The laminar flame speed was obtained using linear extrapolation to zero stretch rate. The measured flame speeds were compared with literature data and numerical predictions using a published detailed kinetic model (Qin, Z., Lissianski, V., Yang, H., Gardiner, W. C., Jr., Davis, S. G., and Wang, H., Proc. Combust. Inst., vol. 28, pp. 1663-1669, 2000). The predictions generally agree well with the experimental data. Both the data and model predictions reveal a quasi-linear relationship between the laminar flame speed and the dilution ratio, contrary to the nonlinear correlations commonly suggested in the literature. The linear dependence issue is numerically extended to include hydrogen and methane flame systems.
机译:丙烷/空气混合物的层流火焰速度是在室温,500 K,650 K和大气压下的较大当量比范围内通过实验确定的。在这些条件下,还针对选定的当量比研究了氮的添加,以模拟废气稀释对层流火焰速度的影响。实验采用了停滞式喷射壁火焰构型,其中通过使用粒子图像测速法获得了流速。使用线性外推至零拉伸速率获得层流火焰速度。使用已发布的详细动力学模型(Qin,Z.,Lissianski,V.,Yang,H.,Gardiner,WC,Jr.,Davis,SG和Wang,H.)将测得的火焰速度与文献数据和数值预测进行比较。 ,Proc.Combust.Inst。,第28卷,第1663-1669页,2000年)。这些预测通常与实验数据非常吻合。数据和模型预测都揭示了层流火焰速度与稀释比之间的准线性关系,这与文献中通常提出的非线性相关性相反。线性相关性问题在数值上扩展到包括氢和甲烷火焰系统。

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