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Instabilities of propagating quasi-2D gaseous flames and chemical fronts in narrow channels.

机译:在狭窄通道中传播准2D气态火焰和化学前沿的不稳定性。

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In order to examine systematically the effects of buoyancy and thermal expansion on propagating fronts, two types of fronts, one having small thermal expansion and one having large thermal expansion, were studied in two-dimensional Hele-Shaw cells (a narrow gap between two flat parallel plates). These cells were used because it is probably the simplest flow apparatus capable of exhibiting buoyancy effects. The small-expansion fronts employed were aqueous Autocatalytic Chemical Reaction fronts that produce propagating fronts, similar to premixed gas flame fronts. The aqueous systems have numerous advantages over gaseous fronts for obtaining fundamental data on the interaction between propagating fronts and buoyancy. These advantages include nearly constant density, nearly constant thermodynamic and transport properties, negligible influence of heat losses, and a high Schmidt number.; Only upward propagating fronts exhibited wrinkling, indicating that buoyancy effects induced wrinkling. A well-defined characteristic wrinkle wavelength was found that was practically independent of the cell thickness and the laminar propagation rate but inversely proportional to the square root of the cosine angle between gravity and the propagating front. The only mechanism consistent with these observations is the presence of an effective surface tension at the interface between product and reactant, which, according to the Saffman-Taylor analysis, will produce a wavelength selection mechanism for buoyantly unstable flows. Correlation between a buoyancy parameter and the wrinkled front speed matched the Yakhot model for the effect of turbulence intensity on turbulent flame speed reasonably well even with no adjustable parameters.; Experiments using gaseous flame fronts were also performed in order to compare with aqueous fronts to assess thermal expansion effects and heat losses. The gaseous flames were composed of CH4 or C3H 8 as fuel, O2 as oxidizer and N2 or CO2 as diluent. Wrinkled fronts were found for all orientations for the gaseous flames. Based on the Joulin-Sivashinsky model, some of the mechanisms that control wrinkling were identified, specifically thermal expansion, viscous fingering and diffusive-thermal effects, which apply only to gaseous fronts. The characteristics of small-scale wrinkling were similar for all orientations but varied with the Lewis number. The characteristics of large-scale wrinkling were buoyancy dominated.
机译:为了系统地检查浮力和热膨胀对传播前沿的影响,在二维Hele-Shaw单元中研究了两种类型的前沿,一种具有较小的热膨胀,另一种具有较大的热膨胀(两个平面之间的狭窄间隙)。平行板)。使用这些单元是因为它可能是能够显示浮力效果的最简单的流动设备。所采用的小膨胀前沿是水性自催化化学反应前沿,其产生传播前沿,类似于预混合气体火焰前沿。水性系统相对于气态前沿具有众多优势,可获取有关传播前沿和浮力之间相互作用的基本数据。这些优点包括几乎恒定的密度,几乎恒定的热力学和传输特性,可忽略的热损失影响以及较高的施密特数。仅向上传播的前沿显示出褶皱,表明浮力效应引起褶皱。发现了明确定义的特征皱纹波长,其实际上与晶胞厚度和层流传播速率无关,但与重力和传播前沿之间的余弦角的平方根成反比。与这些观察结果一致的唯一机理是在产物与反应物之间的界面处存在有效的表面张力,根据Saffman-Taylor分析,该表面张力将为不稳定的浮力产生波长选择机制。浮力参数和褶皱前速度之间的相关性与Yakhot模型相匹配,即使没有可调整的参数,湍流强度对湍流火焰速度的影响也相当好。还进行了使用气态火焰前沿的实验,以便与水性前沿进行比较以评估热膨胀效应和热损失。气态火焰由CH 4 或C 3 H 8 作为燃料,O 2 作为氧化剂和N组成 2 或CO 2 作为稀释剂。在所有方向上都为气体火焰找到了皱纹的锋面。基于Joulin-Sivashinsky模型,确定了一些控制皱纹的机制,特别是热膨胀,粘性指状和扩散热效应,这些机制仅适用于气态前沿。小尺寸起皱的特征在所有方向上都相似,但随路易斯数而变化。大规模起皱的特征以浮力为主。

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