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THE INFLUENCE OF A THERMALLY ACTIVE WALL ON PREMIXED TURBULENT COMBUSTION

机译:热主动壁对湍流燃烧的影响

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A two-scalar description of the thermochemistry of premixed reactants is applied to a turbulent stream impinging on a wall whose temperature is arbitrary. The two scalars are the mass fraction of fuel and the mixture enthalpy. The chemical kinetic characteristics are described in terms of a crossover temperature T~* suggested by activation energy asymptotics and related to the mean rate of strain. The system of describing equations is shown to involve two parameters, one related to the turbulent intensity and a second to the reciprocal of the system Reynolds number. After developing the equations and applicable boundary conditions for arbitrary values of these parameters, their small magnitude in flows of applied interest is exploited in an asymptotic analysis, which leads to the identification of three flow regions and to a reduced set of equations for each region. The location of the flame in these flows depends on the relative chemical kinetic rate, that is, on T~*. If the rate of strain is suitably low, the flame is located in the region most remote from the wall and the wall temperature cannot influence combustion. At increased rates of strain, that is, increased values of T~*, combustion occurs in the second region but the wall temperature again has no influence on combustion provided the wall temperature T(0) is less than T~*. When T(0) exceeds T~*, combustion is confined to the region closest to the wall and these two temperatures and the extent of that combustion as measured by the fuel mass fraction at the wall are related. Thus, we find that the wall temperature influences combustion only if it exceeds the applicable kinetic temperature. Representative numerical results for each region are presented to illustrate these characteristics.
机译:预混反应物的热化学的两标量描述适用于撞击到任意温度壁上的湍流。两个标量是燃料的质量分数和混合物的焓。化学动力学特性用活化能渐近线暗示的交叉温度T〜*来描述,并且与平均应变速率有关。示出的描述方程的系统包括两个参数,一个与湍流强度有关,第二个与系统雷诺数的倒数有关。在开发出这些参数的任意值的方程式和适用的边界条件后,在渐近分析中利用了它们在应用兴趣流中的小幅度,从而确定了三个流动区域,并减少了每个区域的方程组。火焰在这些流中的位置取决于相对化学动力学速率,即T〜*。如果应变率适当地低,则火焰位于最远离壁的区域,并且壁温度不会影响燃烧。在应变率增加时,即T_ *的值增加时,在第二区域中发生燃烧,但是如果壁温度T(0)小于T〜*,则壁温度再次对燃烧没有影响。当T(0)超过T *时,燃烧被限制在最靠近壁的区域,并且这两个温度与该燃烧的程度(通过壁处的燃料质量分数测量)有关。因此,我们发现壁温只有在超过适用的动力学温度时才会影响燃烧。给出每个区域的代表性数值结果以说明这些特征。

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