Experimental and LES investigation of premixed methane/air flame propagating in a tube with a thin obstacle

In this paper, an experimental and numerical investigation of premixed methane/air flame dynamics in a closed combustion vessel with a thin obstacle is described. In the experiment, high-speed video photography and a pressure transducer are used to study the flame shape changes and pressure dynamics. In the numerical simulation, four sub-grid scale viscosity models and three sub-grid scale combustion models are evaluated for their individual prediction compared with the experimental data. High-speed photographs show that the flame propagation process can be divided into five stages: spherical flame, finger-shaped flame, jet flame, mushroom-shaped flame and bidirectional propagation flame. Compared with the other sub-grid scale viscosity models and sub-grid scale combustion models, the dynamic Smagorinsky–Lilly model and the power-law flame wrinkling model are better able to predict the flame behaviour, respectively. Thus, coupling the dynamic Smagorinsky–Lilly model and the power-law flame wrinkling model, the numerical results demonstrate that flame shape change is a purely hydrodynamic phenomenon, and the mushroom-shaped flame and bidirectional propagation flame are the result of flame–vortex interaction. In addition, the transition from “corrugated flamelets” to “thin reaction zones” is observed in the simulation.     

Gas Flow in Porous Media With Klinkenberg Effects

Gas flow in porous media differs from liquid flow because of the large gas compressibility and pressure-dependent effective permeability. The latter effect, named after Klinkenberg, may have significant impact on gas flow behavior, especially in low permeability media, but it has been ignored in most of the previous studies because of the mathematical difficulty in handling the additional nonlinear term in the gas flow governing equation. This paper presents a set of new analytical solutions developed for analyzing steady-state and transient gas flow through porous media including Klinkenberg effects. The analytical solutions are obtained using a new form of gas flow governing equation that incorporates the Klinkenberg effect. Additional analytical solutions for one-, two- and three-dimensional gas flow in porous media could be readily derived by the following solution procedures in this paper. Furthermore, the validity of the conventional assumption used for linearizing the gas flow equation has been examined. A generally applicable procedure has been developed for accurate evaluation of the analytical solutions which use a linearized diffusivity for transient gas flow. As application examples, the new analytical solutions have been used to verify numerical solutions, and to design new laboratory and field testing techniques to determine the Klinkenberg parameters. The proposed laboratory analysis method is also used to analyze data from steady-state flow tests of three core plugs from The Geysers geothermal field. We show that this new approach and the traditional method of Klinkenberg yield similar results of Klinkenberg constants for the laboratory tests; however, the new method allows one to analyze data from both transient and steady-state tests in various flow geometries.     

当量比对汽油燃料两相旋转爆轰发动机工作特性影响实验研究

为了研究当量比对汽油燃料两相旋转爆轰发动机工作特性的影响,开展了以高总温空气为氧化剂的气液两相旋转爆轰实验研究。旋转爆轰发动机环形燃烧室外径、内径和长度分别为202、166和155 mm。汽油和高温空气采用高压雾化喷嘴与环缝对撞喷注的方式混合,以此提高推进剂的掺混效果与活性,采用预爆轰管作为点火装置。实验通过改变汽油质量流量改变推进剂当量比,并基于燃烧室内测得的高频动态压力和平均静压,对气液两相旋转爆轰波的传播模态和传播特性以及发动机的工作特性进行了详细分析。实验结果表明：在当量比为0.79～1.25时,燃烧室内均实现了旋转爆轰波的连续自持传播,且随着当量比的增加,爆轰波传播模态从双波对撞/单波的混合模态转变为单波模态;降低当量比至0.61～0.66,爆轰波传播稳定性变差,传播模态表现为间断爆轰以及零星爆轰;进一步降低当量比至0.53,爆轰波起爆失败。此外,燃烧室平均绝对压力与爆轰波平均传播频率均随着当量比的增加呈先增大后减小的趋势,极大值出现在当量比1.19附近。在此工况下获得了最佳实验结果,旋转爆轰波的平均传播频率为1 900.9 Hz,平均传播速度为1 110.8 m/s,与高频压力信号经快速傅里叶变换得到的主频基本一致,爆轰波传播速度存在严重亏损。

     

?????????????????????????о?

研究了受空气阻尼影响下傅科摆的运动规律,采用数值和解析的方法对其运动轨迹进行 了模拟和讨论,并与无空气阻力时傅科摆的运动进行了比较.     

MORPHOLOGY AND ELEMENTAL COMPOSITION OF DUSTFALL PARTICLES INSIDE EMPEROR QIN＇S TERRA-COTTA WARRIORS AND HORSES MUSEUM

Indoor dusffall samples were collected in Pit 1 and Pit 2 of Emperor Qin＇s Terra-cotta Warriors and Horses Museum in Xi＇an, Shaanxi Province, China. The morphological and elemental analysis for long-term （〉10 years） and short-term （～0.5 year） dusffall particles and lacquer pieces on the faces of partly assembled warriors were performed with scanning electron microscopy with energy dispersive X-ray spectrometer （SEM/EDX）. The results showed that the majority of dusffall samples appeared to be composed of mineral dust particles, fly ash, and biological particles with different elemental compositions. Most of the mineral particles had irregular shapes with smooth edges. Small floccules of calcium sulfate were more frequently observed in long-term dusffall samples than in short-term samples, implying a progressive chemical reaction between continuous dusffall particles and atmospheric sulfur dioxide. Crystals of calcium sulfate were also found near pits on both inner and outer surfaces of lacquer pieces, revealing an acid chemical reaction between sulfur dioxide and lacquer material as the cause of the formation of erosion pits and cracks on surface of lacquer pieces.     

固、液相FAE一次引爆实验研究

基于离散爆轰思想,进行了小药量无约束空间固、液相燃料空气炸药(fuelairexplosive,简称FAE)弹体的野外一次引爆实验。实验结果表明,固、液相FAE弹体的爆炸效果均明显优于等质量的TNT装药;固相FAE弹体一次引爆后的云雾分散规律和爆炸压力场分布不同于液相FAE弹体。在本实验装置条件下,固相FAE弹体的远场超压增长峰值虽未超过等质量的液相FAE弹体,但其火焰持续时间却比等质量液相FAE弹体的长。若仅考察弹体云雾最大半径,固相FAE弹体并不比等质量的液相FAE弹体优越太多,但固相FAE弹体的爆炸作用体积增大较多。     

激波冲击下air/SF6界面的Richtmyer-Meshkov不稳定性

实验研究了低马赫数(1.27)激波作用air/SF6界面的RM不稳定性问题.air/SF6初始正弦界面由厚度为1～2 μm的薄膜相隔得到,用阴影法测试界面演化过程.实验结果表明:由于不稳定性重流体(SF6)向轻流体(air)演化成“尖钉”结构,而轻流体演化为“气泡”结构;由于界面切向速度差的Kelvin-Helm-ho...     

风速对室内气流分布影响的数值仿真

对低温空调系统送风特性进行了研究,着重于低温送风空气流动状况及其对室内环境的影响.以某一典型的空调房间为研究目标,利用计算流体动力学(CFD),研究在低温送风条件下,室内气流组织的分布状况.通过建立合理的数学模型进行数值模拟,运用试验手段验证了模拟结果的可靠性,得到几种送风速度下的室内气流速度场与温度场的计算结果.经过分析,确定该空调室的送风速度范围与最佳值.最后得出每一种低温送风系统对应着一定的送风速度范围的结论.     

室内惯性/视觉组合导航地面图像分割算法

导航技术是机器人实现自主移动的关键技术之一。针对惯性导航创建全局导航地图困难等问题,提出一种新的惯性/视觉组合导航室内全局地图创建方法。规定机器人只能在地面区域中移动,并利用室内俯视图像建立全局地图,提出一种俯视图像地面区域的自动分割算法。首先,利用主元分析算法对图像的局部颜色特征进行降维;其次,利用聚类算法对地面区域进行自动分割;最后,建立了室内俯视图像数据库并对算法的性能进行了验证。由于第四组图像中包含反光区域,算法的分割结果较差,平均正确分辨率为75%。算法在其他各组的平均正确分割率为85%左右。为提高算法的性能,可在应用本算法前利用反光区域检测算法对图像进行预处理。     

爆炸荷载下沉箱重力式码头模型毁伤效应

在野外条件下开展了不同爆炸荷载条件下沉箱重力式码头模型毁伤效应实验,得到了沉箱重力式码头模型在1 kg TNT当量空中爆炸、水下爆炸以及结构内部爆炸后的毁伤模式,并针对不同毁伤模式给出了相应的抢修建议。实验结果表明：空中爆炸荷载下码头仅面板局部破坏形成爆坑;水下爆炸荷载下码头迎爆面及相近区域形成大量裂缝;结构内部爆炸荷载下码头仓格大变形破坏且中间面板被掀飞;从横向对比来看,在相同爆炸当量下空中爆炸荷载下码头毁伤程度最小,结构内部爆炸荷载下码头毁伤程度最大。