Influence of rarefaction wave on premixed flame structure and propagation behavior

To explore the influence of rarefaction wave on the structure and propagation behavior of the premixed propane/air flame in a rectangle combustion pipe, the techniques of high speed Schlieren photograph method, pressure measurement and so on are used to study the interaction processes between rarefaction wave and flame. Two cases of rarefaction wave-flame interaction were performed in the experiment. The experimental result shows that both the rarefaction waves can cause the flame transition from laminar to turbulent combustion quickly. The cowflow rarefaction wave decreases the flame speed, while the counterflow rarefaction wave leads the flame propagation speed to increasing on the whole, accompanied with sharp vibration.     

“变截面管中跨声速气流”一文引理的证明

本文对T·P·Liu教授关于“变截面管中跨声速气流”一文的关键性引理给出一个清楚的证明,以使这篇有影响的开创性论文更加完美。     

一类三维Burgers方程的解

求出一类三维拟线性微分方程的非自模形式的三维激波、稀疏波及其整体相互作用的结构．对于任意一固定时刻t，得到两种解分别具有特殊的结构．     

Influence of rarefaction wave on premixed flame structure and propagation behavior

To explore the influence of rarefaction wave on the structure and propagation behavior of the premixed propane/air flame in a rectangle combustion pipe, the techniques of high speed Schlieren photograph method, pressure measurement and so on are used to study the interaction processes between rarefaction wave and flame. Two cases of rarefaction wave-flame interaction were performed in the experiment. The experimental result shows that both the rarefaction waves can cause the flame transition from laminar to turbulent combustion quickly. The cowflow rarefaction wave decreases the flame speed, while the counterflow rarefaction wave leads the flame propagation speed to increasing on the whole, accompanied with sharp vibration.     

ASYMPTOTIC STABILITY OF SOLUTION TO THE INITIAL-BOUNDARY VALUE PROBLEM FOR SCALAR VISCOUS CONSERVATION LAWS CORRESPONDING TO RAREFACTION WAVES

1.IntroductionWeconsidertheinitial-boundaryvalueproblem(IBVP)forscalarviscousconservationlaw(ut f(u).=uxx,xE(0, co)=R ,t>0,o,(n \--9,ifI~9,f~M(IBVP){u(0't)=u~(t)-1~i---t:7),[u(x,0)=u000={=:0)f:LO .,wheref"(u)>0foralluunderconsideration,andu--u (1.1),andu~(t)~u~EL'(R ),U'(t)EL'(R ).(1.2)Undercondition(1.l)or(l.l)',thecorrespondingRiemannproblem{;;ot:<:>;i,>=x{,:3'f:,:(13)yieldstherarefaCtionwavesolution(u~)x5f'(u~)t,r"(X,t)=17j,)~1(…     

微气体螺旋槽推力轴承-转子系统非线性动力学分析

基于分子气体膜润滑模型探讨微气体螺旋槽推力轴承中的稀薄效应,将广义雷诺方程与运动学方程在时域内耦合并采用直接数值模拟方法联立求解,获得了任意时刻微转子的瞬态位移和速度响应,考察了气体稀薄效应以及不同螺旋槽结构参数对微气体螺旋槽推力轴承-转子系统非线性动力学行为的影响,并得到不同转速对应的轴向扰动临界值.结果表明:考虑稀薄效应时微轴承-转子系统显示出更好的稳定性;转速增加,轴向扰动临界值降低;能提高微轴承承载力的最佳螺旋槽结构参数,并不利于提高微系统的稳定性.     

微通道内气体流动参数化数值模拟

基于ANSYS Fluent软件,对微通道内气体在不同压力驱动下的流动做参数化数值模拟分析,得出不同克努森数(Kn)的通道出口截面速度分布图和质量流率,并将仿真结果和理论研究进行比较,分析微通道内气体流动特性与宏观流动的异同,研究稀薄气体效应.模拟结果表明:在微通道中,连续介质假设失效;当微系统特征尺度很小或者工作压力很小时,微通道内的气体具有较大的Kn,出现明显的稀薄气体效应;Kn越大,稀薄气体效应越强烈;稀薄气体效应导致固壁边界的滑移速度和质量流率变大.     

液体爆炸分散过程中界面破碎的实验研究

设计了一种有上下平面约束的液体爆炸分散装置, 通过阴影照相获得气液界面破碎形态变化的时间序列, 并应用平面激光诱导荧光(PLIF)得到了径向膨胀液体环内诱导的荧光照片. 采用二维图像处理、分形几何和数值模拟相结合的方法, 较系统地分析了实验结果. 最后, 讨论了液体环及其气液界面运动数学模型建立中的问题.     

等熵情形下同向疏散波和激波的相互作用问题

对于1维等熵情形,利用激波极线和特征轨线,对同向疏散波和激波相互作用的结果进行了分析,得到了相互作用结束后受干扰的波和反射波的性质及其与初始时刻疏散波和激波相对强度之间的关系.另外,利用Riemann不变量以及各物理量之间的依赖关系和变化趋势给出了相互作用区域内特征族的形态.