Large Eddy Simulations of a piloted lean premix jet flame using finite-rate chemistry

A Large Eddy Simulation (LES) model capable of accurately representing finite-rate chemistry effects in turbulent premixed combustion is presented. The LES computations use finite-rate chemistry and implicit LES combustion modelling to simulate an experimentally well-documented lean-premixed jet flame stabilized by a stoichiometric pilot. The validity of the implicit LES assumption is discussed and criteria are expressed in terms of subgrid scale Damköhler and Karlovitz numbers. Simulation results are compared to experimental data for velocity, temperature and species mass fractions of CH₄, CO and OH. The simulation results highlight the validity and capability of the present approach for the flame and in general the combustion regime examined. A sensitivity analysis to the choice of the finite-rate chemistry mechanism is reported, this analysis indicates that the one and two-step global reaction mechanisms evaluated fail to capture the reaction layer with sufficient accuracy, while a 20-species skeletal mechanism reproduces the experimental observations accurately including the key finite-rate chemistry indicators CO and OH. The LES results are shown to be grid insensitive and that the grid resolution within the bounds examined is far less important compared to the sensitivity of the finite-rate chemistry representation. The results are analyzed in terms of the flame dynamics and it is shown that intense small scale mixing (high Karlovitz number) between the pilot and the jet is an important mechanism for the stabilization of the flame.     

电场驱动直射流的动量方程

给出了电场驱动直射流的一维动量守恒方程．该方程是用应力分量表示的,适用于任何流体本构关系,只要流体是不可压缩的．结果显示,为了使方程封闭,需要沿轴向和径向两个方向的本构关系．然而,当附加应力张量的迹为0时,只需要沿轴向的一个本构关系就足够了．还发现,射流的第二主应力差的零阶近似总为0．与其他类型的动量方程做了比较．     

横观各向同性介质中椭圆夹杂受非弹性剪切变形引起的弹性场的确定

本文求解了横观各向同性介质中椭圆夹杂内受非弹性剪切变形引起的弹性场。采用各向异性弹性力学平面问题的复变函数解法，结合保角变换，获得夹杂内应变能和基体内边界的应力分布和相应的应变能的表达式。进一步，根据最小应变能原理，获得表征夹杂平衡边界的两个特征剪切应变，从而得到了弹性场的解析解。通过应力转换关系，验证了应力解满足夹杂边界上法向正应力和剪应力的连续条件，表明了该解的正确性。本文解可用于复合材料断裂强度的分析中。