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1.
Turbulent combustion remains to be one of most complicated technologies due to the complexities of turbulence and combustion as well as the interaction of both.This paper presents a vitiated cofiow combustor, which is newly used for the fundamental research into turbulent combustion. The characteristics of controllable active thermo-atmosphere (CATA) of a vitiated coflow combustor are investigated. The results show that the oxygen mole frac tion of vitiated coflow flames between 0% and 21% yield coflow temperature between 700 and 1500 K, and there is a constant temperature space as a cylinder with a radius of 40mm. These features of the vitiated coflow indicate the existence of a controllable active thermo-atmosphere, which benefits the basic study on the autoignition of a combustible mixture in a homogeneous charge compression ignition (HCCI) combustion.  相似文献   

2.
Direct numerical simulation of a particle-laden weak-shearing plane jet   总被引:1,自引:0,他引:1  
Direct numerical simulation (DNS) has been utilized to solve numerically a two-dimensional compressible weak-shearing plane jet, in which the jet exit velocity and the co-flow velocity are in the same magnitude (2∶1 in this paper). We also use the one-way coupling method to simulate the dispersion behaviors of solid particles in various representative sizes, i.e. St=0.01, 1, 10, 100, where St is the Stokes number. We get a vorticity field with fully varicose (symmetrical) modes and the entire precise processes of the rolling-up of one spanwise vortex, the pairing of two vortexes and the mixing of three vortexes. The mean longitudinal velocity (U) profile compares well against the experimental results. The Reynolds stress profile looks special due to the symmetrical vorticity field. The particles whose St=0.01 reproduce the vortex structures in detail, and the ones of St=1 exhibit interesting self-organized behaviors and possess the most non-uniform concentration field. They disperse uniformly around the single and pairing vortex kernels, while a few of them are arranged almost in a straight line in the center region of the paring vortexes, which is caused by the contribution of the border of two vortexes in the pairing process. St=10 and 100 can be treated as large particles, on which the flow field has few impacts.  相似文献   

3.
Conditional moment closure modeling of a lifted turbulent flame   总被引:3,自引:1,他引:3  
The problems about reacting turbulent flows are made difficult because the rates of reaction of concern are highly nonlinear functions of reactive scalars. The turbu-lence in the flow engenders mixing of non-uniformities in species and temperature, and the rates of this mixing are usually not fast compared with the rates of reaction. As a consequence, large spatial and temporal fluctuations occur in the scalar quantities and efforts to express average rates of reaction in terms of average valu…  相似文献   

4.
为避免火焰穿透防火舱密封造成额外安全风险,对防火实验用油燃烧器火焰的射流传热特性进行了研究,根据传热分析和实测温度探索了防火墙导热的温度变化规律。在分析波纹套密封防火实验失败原因后,通过选择合适硅橡胶材料,进行特殊纤维铺层布置,增设了轻质隔热垫,实验验证了隔热垫厚度(层数)和面积对隔热效果的影响。研究表明:无隔热防火墙过余温度在初始非定常阶段呈指数增长,高温导致波纹套根部自燃。芳纶1313纤维可促进硅胶形成致密强韧的绝热壳,织物界面可造成耗能的湍流,能有效隔热,同时通过覆盖足够面积花瓣式内孔的多层隔热垫,增加热阻,可明显降低背温实现柔性密封防火。  相似文献   

5.
Direct numerical simulation is employed to investigate the premixed jet flame of methane in lean, combined with a detailed chemical kinetics including 17 species and 58 elemental steps and distinct Lewis numbers. Cold methane-air mixture at 0.55 equivalence ratio is injected into the coflow area with 9500 Reynolds number. The coflow ambient gas is set to be the burnt gas of the methane-air mixture in main jet and temperature is assigned to be the corresponding adiabatic flame temperature 1515 K. The whole s...  相似文献   

6.
为研究瓦斯燃烧器的火焰特性 ,采用k ε湍流模型、三气体扩散燃烧模型及综合辐射模型 ,对旋流稳焰瓦斯燃烧器湍流扩散火焰进行了数值模拟。研究结果表明 ,在旋流作用下 ,在火盆及其前端附近区域内形成了中心回流区 ,使燃气与助燃空气在此处发生剧烈掺混而被点燃 ,这有利于火焰稳定。在火焰前端仍存在一个高温尾流区 ,在选用和设计燃烧器时应充分考虑这一现象。燃气喷孔直径对火焰长度的影响非常显著 ,喷头顶部气孔位置和火盆锥口角对火焰长度影响较小。随着空气过剩系数和燃气中空气含量的增加 ,火焰长度明显减小。在实际应用中 ,应充分考虑燃烧器结构和操作条件的影响 ,以提高加热炉的效率和安全性。  相似文献   

7.
在高超速情况下,利用直接数值模拟方法,我们研究了真实气体效应(振动由度激发导致比热随温度变化)对槽道湍流影响,并与不考虑振动由度激发情况进行了比较.我们发现振动能激发对统计平均量影响主要体现在温度上,它能够抑制湍流场中平均温度升高;而对于密度,速度及压强影响很小.振动由度激发使原分运动更加剧烈,以致湍流场趋于平坦,表现为脉动值、相关函数及互相关函数减小.同时,由于振动能激发过程是一个吸热过程,因此它对湍流有抑制作用,表现在减小涡量、抑制湍能成及耗散等方面.振动由度激发对于湍流两点相关量、偏斜因及平坦因影响很小.  相似文献   

8.
针对气固圆湍射流流动采用基于双向耦合的大涡模拟方法进行了模拟,研究了直径为105μm的颗粒的存在对圆湍射流的影响。单相流动的预报结果在射流形态以及时均速度和湍流强度等统计结果方面均与实验结果符合良好。两相流动的时均速度和湍流强度等统计结果与实验结果符合较好,与单相流动的模拟结果相比,105μm的颗粒加入流场后,由于其较快的响应特征起到了阻尼作用,从而降低了气相场的湍流强度。  相似文献   

9.
平面自由湍射流拟序结构的大涡模拟研究   总被引:2,自引:0,他引:2  
对空间发展的平面不可压缩湍射流拟序结构的非定常演化过程进行了大涡模拟。采用标志物浓度等值线分布示踪平面射流气相流动 ,Reynolds数为 1130 0 ,模拟结果再现了平面射流中 Kelvin- Helm holtz不稳定性的发生以及展向大尺度涡的卷起、合并、破碎过程。捕获到了射流拟序结构剧烈相互作用的“偶极子”和“三极子”现象。在拟序结构的配对过程中 ,大尺度旋涡的尾迹混合形成了流向“发卡”型拟序涡结构。平面射流拟序结构的时空演化过程所呈现出的卡门涡街特征主要集中于初始段的后部和过渡段的前端。数值流场显示结果和染线法的实验结果吻合得很好  相似文献   

10.
基于直接数值模拟方法和详细化学反应机理研究了流体动力学不稳定性和热-质扩散不稳定性共同作用下的低热值气体燃料掺氢胞状火焰的发展和演变过程.建立了多组分气体燃料燃烧控制方程,获得了不稳定性作用下的低热值气体燃料掺氢胞状火焰的多种演变形式:胞的分裂、局部熄灭、二次熄灭和再燃.研究结果表明随着燃料中H2的增加,胞状火焰出现的时间提前,火焰胞的幅值增加.随着燃料中CO2的增加,火焰的不稳定性受到抑制.低热值气体燃料掺氢火焰在不稳定时会出现火焰胞的分裂、局部熄灭和再燃等3种动力学形态.胞的二次熄灭只发生在热-质扩散不稳定性较强的稀燃H2/空气火焰中.  相似文献   

11.
Lean premixed flame characteristics of several typical low calorific value (LCV) syngases (basis CO/H2/CH4/CO2/N2),including bituminous coal,wood residue,corn core,and wheat straw gasification syngas,were investigated using OH planar laser induced fluorescence (PLIF) technology.OH radical distributions within the turbulent flame were measured for different turbulence intensities.Flame structures of syngases were analyzed and characterized with respect to burnt and unburnt regions,flame curvature (sharp cusp),local extinction (holes and penetration),OH reaction layer thickness,wrinkling,and other features,with OH-PLIF instantaneous images and statistical analysis.Results show that H2 content,LCV,and turbulence intensity are the most effective factors influencing the OH radical intensity and thickness of OH radical layers.The bituminous coal gasification syngas with relatively higher LCV and H2 content tends to burn out easily.Through changes in thickness of the OH radical layers and signal intensities,the reaction layer can be compressed by intensifying turbulence and thereby the combustion processes of syngas.  相似文献   

12.
采用谱方法求解柱坐标系下三维不可压缩流Navier-Stokes方程,直接数值模拟了不同半径比下的同心旋转圆筒间的Taylor-Couette(TC)湍流问题.由于TC湍流是由大尺度Taylor涡和湍流随机脉动的叠加而成,采用周向平均成功识别了TC湍流中的大尺度Taylor涡,并将其诱导的脉动流动与湍流随机脉动分离开来,对比分析了不同半径比下大尺度Taylor涡对脉动强度和湍动能的贡献;同时,通过计算雷诺应力输运方程,研究了半径比对湍动能生成、耗散和再分配等动力学特性的影响.计算结果表明,在小半径比的宽槽TC湍流中,Taylor涡诱导的脉动流相对较弱,湍流随机脉动更为强烈,其对湍流统计特性的影响占优;在大半径比的窄槽TC湍流中,流体脉动特性主要源于Taylor涡的贡献;另外,随着半径比的增大,近外壁面附近流体沿周向剪切作用增强,流场表现出类似于平板Couette流的流动特性.  相似文献   

13.
Lean premixed flame characteristics of several typical low calorific value (LCV) syngases (basis CO/H2/CH4/CO2/N2),including bituminous coal,wood residue,corn core,and wheat straw gasification syngas,were investigated using OH planar laser induced fluorescence (PLIF) technology.OH radical distributions within the turbulent flame were measured for different turbulence intensities.Flame structures of syngases were analyzed and characterized with respect to burnt and unburnt regions,flame curvature (sharp cusp...  相似文献   

14.
采用大涡数学模型对横流环境下正弦振荡射流进行三维模拟,重点分析了横流环境下非振荡射流与振荡射流运动特性和稀释规律的差异,并探讨了振荡参数对射流的影响.结果表明:横流环境下振荡射流形态与非振荡射流区别明显,其运动轨迹发生弯曲,呈现出明显的间歇性污染物云团现象;与非振荡射流相比,振荡射流的冲击高度与弯曲程度明显增加,与周围...  相似文献   

15.
The coherent structures of a three-dimensional temporally mixing layer and the associated dispersion patterns of particles are numerically studied using a pseudospectral method for fluid and the Lagrangian approach for tracing particles at different Stokes numbers without consideration of particle-particle interactions. The results show that the particles with Stokes number of the order of unity have the largest concentration near the outer edges of the large-scale spanwise vortex structures. The study validates the effect of the streamwise large-scale structures on the particle distribution along the spanwise and transverse directions and it enhances with the development of the three-dimensionality of the mixing layer, which results in a ‘mushroom’ shape of the particle distribution in the spanwise direction.  相似文献   

16.
运用大涡模拟方法分别对不加扰动和加扰动的圆湍射流流动进行了数值模拟,比较了两者在大尺度涡结构的演化过程以及时均速度和湍流强度等统计结果方面的预报差异,并与实验结果进行了对照。模拟结果表明,施加了入口扰动的模拟结果在物理真实性方面和统计结果的准确性方面均要明显优于未加扰动的模拟结果。分析了不加扰动和加扰动模拟的本质差异,指出准确预报实际圆湍射流流动应采用施加入口扰动的三维模拟。  相似文献   

17.
采用大涡模拟方法数值模拟了流向椭圆喷嘴的湍流横向射流,重点研究其旋涡结构的产生、发展等动力学演化过程.结果表明:文献中所报道的横向射流基本涡结构,如反向旋转涡对、前缘涡、后缘涡、悬涡、肾涡、反肾涡等并非独立的物理实体,而是分别对应于新发现的横向射流基本涡结构——起始于喷嘴的三维拉伸涡环的局部结构.  相似文献   

18.
为了解火焰法合成纳米颗粒过程中流体力学和颗粒动力学作用过程,利用CFD商业软件FLUENT模拟了在湍流扩散火焰中合成TiO2纳米颗粒的过程.模型在没有考虑先驱物TiCl4反应的情况下,计算了在燃烧室内的速度场和温度场.假设当气体温度超过一定数值后,所有先驱物分子迅速转化为TiO2单分子;引入Kruis的颗粒动力学模型对产物颗粒直径、比表面积等进行了预测,研究了不同的火焰结构对其性质的影响,并分析其形成原因.结果表明颗粒的烧结特征,即温度是影响一级颗粒及聚集块尺寸的关键因素;火焰温度越高,聚集块中一级颗粒的数目增长得越快,出口处一级颗粒及聚集块的尺寸也就越大.  相似文献   

19.
为研究后混合水射流喷丸喷头内部两相流的运动规律,采用FLUENT软件对其内部液固两相流场进行数值模拟。根据其流动特性,数学模型采用欧拉模型,湍流模型采用标准的k-ε模型,并将固体相看作拟流体,分析喷丸压力和靶距对轴向速度和轴向动压强的影响。结果表明:喷头内的轴向速度和轴向动压强的变化规律是相似的,并且在相同的喷丸条件下,水流场的轴向速度大于弹丸流场的轴向速度,水流场的轴向动压强小于弹丸流场的轴向动压强。当喷丸压力为10MPa、靶距为55 mm时,水流场和弹丸流场在弹丸喷嘴出口处的轴向速度分别为63.3和56.9 m/s,水流场和弹丸流场在弹丸喷嘴出口处的轴向动压强分别为1.97和3.94 MPa。  相似文献   

20.
为考察预混火焰面附近的湍流特性,以及湍流与化学反应相互作用的机理,采用激光多普勒技术(laser Doppler anemometry,LDA)对本生火焰和V型火焰的流场进行了诊断。分别通过固体粉末和雾化硅油液滴进行无条件和条件示踪,研究了全场及反应物来流的流动特性。无条件示踪的测量结果表明,火焰区的流场存在湍流度迅速增大然后衰减的现象,而速度的测值呈现双峰分布。条件示踪测量结果表明,在火焰区内反应物来流的流动特性并没有发生明显的改变。在剪切流场中,火焰面的脉动和皱褶不显著影响上游反应物的流动特性。  相似文献   

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