浆体管道输送水击压力波波速的探讨

 在考虑自由气体存在的影响下，推导出浆体水击压力波波速的 计算公式.分析表明很少量的气体存在会使波速明显降低. 气体体积 浓度较大时波速随浆体浓度的增大而减小，重质物料的减小趋势较 为明显；气体体积浓度较小时轻质物料波速随浓度的增加而增加. 相同条件下非均质流波速比伪均质流波速大，两者差异主要受浆体 中固体物料的密度和浆体体积浓度影响. 考虑气体影响作用的浆击 波速计算值与实测结果更吻合.     

浆体管道内静止圆柱状型料的起动

在动量定理和能量定理的基础上,建立静止圆柱状型料在浆体管道内起动的动量方程和能量方程,并由此导出静止型料在浆体管道内的起动速度计算公式．经型料管道起动实验验证,该公式较好地描述了静止型料在浆体管道中开始起动的物理条件,能有效地推断和预测静止型料在浆体管道流中的起动速度．理论计算值和实验数据指出,静止型料在浆体管道内的起动速度,不仅和管道平均流速紧密相关,而且和浆体密度、型料形状比以及型料管道直径比紧密相关．     

管内固-液两相流动阻力特性影响因素的敏感性分析

在浆体管道的工程设计中，管道阻力损失是一项关键参数。在大量实验的基础上，本文根据取得的有关实验成果，对影响管内固-液两相流动阻力的4个最主要因素-管径D、颗粒比重S、浆体浓度Cv和倾角θ进行了深入探讨，并采用多因素分析法比较了它们对于固体物料管道水力输送阻力输送阻力损失的影响程度大小关系，从而为在工程设计降低管道输送阻力提供了主要调整手段。     

不同浓度粉煤灰浆体管内流动规律试验研究

粉煤灰浆体在矿山及地下工程中的使用越来越广泛,而其管道运输时的过渡流速、屈服应力衰减规律及紊流水力坡度方面的研究还略显不足,开展这方面的研究有重要的应用价值。为此本文进行了体积浓度为0.422、0.441、0.462和0.492的粉煤灰浆体在直径为0.0627m和0.0777m的水平管道中流动输送试验研究,通过试验数据分析,给出了浆体从层流到紊流的过渡流速值,结合前人研究成果,给出了浆体过渡流速计算公式。同时通过分析浆体切应力和切变率曲线,发现粉煤灰浆体流型为宾汉体。通过试验数据拟合法,给出了宾汉体屈服应力衰减系数与相对流速偏移量关系的表达式,由此给出了宾汉流体紊流水力坡度计算模型。对比结果表明,模型计算值与实测值最大偏差为9.42%。     

气液两相流压力波传播速度研究

将双流体模型用于绝热无相的管道气液两相流,依据小扰动线化分析原理,导出了压力波波数Ｋ方程通过对不同空隙率下肉体上压力波小随角频率变化的计算,研究了虚拟质量力和狭义相间阻力对压力波波速及其人色散性的影响。对泡状流和弹状流压力波波速的计算结果与前人的测量结果作了比较,两者符合良好。     

水下欠膨胀高速气体射流的实验研究

采用实验途径研究了下水高速气体射流的动力学特性,研制了水下高速气体射流实验系统并发展了相应的测试手段。实验中,用插入式静压探针测量了射流轴线静压分布;用γ射线衰减法测量了径向空隙率分布,从而揭示了水下高速气体射流均压和掺混两个过程的基本规律。测量结果表明：水下高速气体射流在欠膨胀工况下运行时,近场将出现含有复杂波系结构的膨胀压缩区域,由于气水的掺混作用,水下欠膨胀气体射流均压化过程比空气中衰减得快。测量结果还表明,水下射流在近场区的混合层由气水两相占据,其流态从靠近气体侧的液滴流型过渡到靠近液体侧的气泡流型。     

水锤作用下管路系统支撑处位移与输送速度的关系

以深海采矿扬矿垂直输送硬管在水力输送过程中的管道为研究对象,分析了管道系统在水锤冲击下考虑泊松耦合时流体和结构的瞬态响应;建立了管道系统在瞬变流情况下的流固耦合模型,获得了弱约束条件下支撑处管道位移随输送速度的变化关系。结果表明:随着输送速度的提高,当管道输送系统发生水击现象时,压力发生剧烈变化,导致管道支撑点处X、Y、Z三个方向的位移均大幅增加;X、Y方向位移呈现对称性,由于Z方向与轴向一致,水击发生时其位移变化较小;随着时间的延续,Z方向位移变化愈发明显;当采用较高输送速度输送矿石浆体时,管道与两相流浆体相耦合的振幅较大。以上结果可为管道设计中的支撑结构设计提供参考。     

管道液体流速对超声导波纵向模态传播的影响分析

建立了充液管道中液体流动时超声导波纵向模态的群速度频散方程,研究了模态、激励频率对载流管道内超声导波传播的影响。在数值仿真的基础上,利用环形压电阵列在载流管道中激励接收频率305kHz的L(0,5)模态,对纵向模态在载流管道中的传播特性进行了实验研究。研究结果表明,载流管道内频率305kHz的L(0,5)模态的群速度与液体流速呈近似线性变化。实验结果与理论分析结果相符,该结论为载流管道流量在线测量提供了一种新方法,为超声导波流量计的研制打下了理论基础。     

液固流动理论的进展

1.引言研究液固悬浮体的意义在于应用这种研究成果,通过长距离管道输送悬浮体来输送固体颗粒,并使动力消耗合理、单价较低.与气体输送即气力输送相比,在相似的温度以及有效的工作压力下,同样的固体颗粒最小悬浮速度以及压降在液体中比在气体中要低得多。这      

气泡-水流两相流的激光多普勒法测量

为区分激光多普勒稀态两相流动测量中出现的流体相信号和颗粒(气泡、液滴)相信号,本文提出可见度和基座的复合判别法,并设计了专用的信号预处理器,此预处理器能将原始多普勒信号分为两路,分别代表两相,并可用计数型信号处理器测量每路的速度及其它统计量。使用本方案对矩形管道內低速气泡-水两相流的实验和测量表明,对两相的区分和测量是成功的。文中给出了两相速度、湍流度和气泡滑移速度的测量结果。     

Slurry flow metering by pressure differential devices

A simple system for measuring slurry concentrations and flow rates by pressure difference devices has been studied. Solids concentrations have been determined by pressure measurements in vertically upwards and downwards sections of the flow, and flow rates measured by a venturi meter located alternately in horizontal, vertically upwards and vertically downwards flows. The venturi performance has been described in terms of a discharge coefficient based on mixture density, and the concentration measurements have been compared to values determined by weigh tank samples. A range of sand slurries with median particle size from 150 to 740μm and an ilmenite slurry with a median particle size of 170μm have been tested. A limited number of tests on a 17μm sand slurry have also been recorded.For fine sand slurries (150μm or below) it was found that the water value of venturi-discharge coefficient applied, so that the accuracy of flow measurements will be limited only by the accuracy of the pressure and specific weight measurements. Experimental values of specific weight from the vertical loop section were on average within 1% of the values from the weigh tank, where the majority of this scatter was caused by the limitations of the weigh tank method.For coarser slurries, the venturi-discharge coefficients depended primarily on solids concentration, with a secondary dependence on Reynolds number, and values were below the water value. An analysis of the flow based on a one-dimensional momentum balance indicated that relative velocity between the phases could account for these low values of discharge coefficient. This was verified by high-speed photography of the flow which suggested a movement of particles towards the centre of the flow at the throat.The overall indications are that the combination of a vertical loop section of flow (for concentration or specific weight measurements) and a venturi meter (for flow rates) provides a simple and accurate means of metering slurry flows. For fine slurries only water calibrations or calibrations from Standards are required.     

Ideal Gas Outflow from a Cylindrical or Spherical Source into a Vacuum

The solutions of initial and boundary value problems of the outflow of an ideal (inviscid and non-heat-conducting) gas from cylindrical and spherical sources into a vacuum are obtained. Time is measured from the moment, when the source is turned on; at this moment the source is surrounded by a vacuum. The entropy, flow rate, and the Mach number of the gas outflowing from the source are given, together with the source radius; the Mach number can be greater of or equal to unity. If the source radius is greater than zero, then the flow domain in the “radial coordinate–time” plane consists of the stationary source flow and adjoining non-self-similar centered expansion wave consisting of C^?-characteristics. The stationary flow is described by the known formulas, while the expansion wave is calculated by the method of characteristics. The calculations by this method confirm the earlier obtained laws for large values of the radial coordinate. The interface between the vacuum and the expansion wave is the straight trajectory of particles and, at the same time, a unique rectilinear C^?-characteristic. For the source of zero radius (“pointwise” source) the velocity, density, and speed of sound of the outflowing gas are infinite. The gas velocity remains infinite everywhere, while the density and speed of sound become zero for any non-zero values of the radial coordinate. For the pointwise source the problem of outflow into a vacuum is self-similar. In the plane of the “self-similar” velocity and speed of sound its solution is given by three singular points of a differential equation in these variables. At one of these points the self-similar velocity is infinite, the self-similar speed of sound is zero, and the self-similar independent variable varies from zero to infinity, with the exception of the extreme values.     

地震和波流作用下海底悬跨管线模型实验研究

利用水下地震-波流联合模拟实验系统研究了海底管线在波浪、水流和地震作用下的动态响应特征。实验中考虑了有无地震作用、悬跨长度、波浪高度、水深、水流速度以及是否满管状态等因素。通过DDP动态数据后处理软件对实验结果进行处理分析,得到海底悬跨管道的动态响应特性。实验结果表明:在浅海海域,悬跨管线的动态反应受波浪及水深变化的影响不明显,悬跨长度是影响管道动态响应的主要影响因素;悬跨管线在地震与波流共同作用下的反应与仅地震作用下的应变存在差别;在波浪力作用下,空管时管线的应变要小于满管时的情况。     

Numerical modelling and computation of fluid pressure transients with air entrainment in pumping installations

In pumping installations such as sewage pumping stations, where gas content and air entrainment exist, the computation of fluid pressure transients in pipelines becomes grossly inaccurate when a constant wave speed is assumed. An accurate numerical model with gas release and absorption has been developed in this paper and used to compute the fluid pressure transients in the pumping mains of selected pumping installations. Free and dissolved gases in the transported fluid and cavitation at vapour pressure are also modelled. When compared with the gas-free case, computations show that entrained, entrapped or released gases amplify the positive pressure peak, increase surge damping and produce asymmetric pressure surges. While the upsurge with air entrainment in the pipelines was considerably amplified, the downsurge was only marginally reduced. The computed results show good agreement with the data available.     

Pressure waves in a separated gas-liquid layer in a horizontal duct with a step

Pressure wave propagation into a separated gas-liquid layer in a horizontal duct with a step is investigated analytically. The linear solution is derived assuming a large density ratio of liquid to gas. The solution can be found first for the gas layer and then for the liquid layer. The linear wave in a liquid layer is valid even for fairly large initial pressure ratios, and clearly exhibits the dispersive characteristics of the pressure wave in a liquid layer. As the initial pressure ratio is increased, the pressure wave in the gas layer becomes a shock wave. Thus, its effect on the wave in a liquid layer can be found analytically by modifying the boundary condition in part. The wave in a liquid layer consists of a main wave, which propagates with the shock speed in gas, and a precursor wave, whose front propagates with the speed of sound in liquid. The precursor wave has an oscillatory structure; its amplitude increases with increasing shock strength and also with liquid layer thickness.     

Phase and signal velocities of waves in dissipative media. Special relativistic theory

The signal and phase velocities (and their frequency dependence) for all possible plane waves in a relativistic gas (of molecules or photons) with dissipation have been determined from the linearized relativistic 13-moment theory. For each direction in 3-space, and for each frequency, one transverse and two longitudinal waves were found. (In addition, some waves are associated with the mass flow and have the mass flow speed.) Of the longitudinal waves, the fast one is a pressure (sound) wave. It is accompanied by a slow longitudinal thermal dissipation wave and a transverse viscous dissipation wave. The pressure wave has a velocity larger than the Laplace adiabatic speed of sound, while the two dissipation waves have a velocity less than the Laplace speed. All the speeds have been expressed explicitly in terms of quantities associated with the state of equilibrium which existed before passage of the wave. It has also been shown that in the ultrarelativistic limit (extremely high temperatures) all signal speeds remain less than the speed of light in vacuo.The major part of this article was presented at the Seminar on Natural Philosophy at The Johns Hopkins University, Baltimore, on November 24, 1971.     

颗粒材料中致密波结构研究

采用一维两相流模型与相应颗粒构形应力函数,研究了致密波的形成及其结构．用简化两相流模型系统地讨论致密波对有关因素的依赖关系．分析指出：小于基体材料音速的致密波仅能在非理想颗粒材料中存在,从波前到波后,所有状态物理量光滑过渡．大于基体材料音速的致密波,波头可能存在间断．应力函数与致密粘性确定后,致密波速度决定致密波结构、宽度、终态压实度．采用一维两相流模型模拟了活塞驱动颗粒床形成致密波这一动态过程．用线方法（MOL）对该方程组求数值解．计算表明,经过短暂的非稳态过程,颗粒床中形成一稳态致密波．分析了活塞速度与初始孔隙率对致密波结构的影响,并对简化两相流模型与两相流模型的计算结果进行了对比．     

浅埋高压输气管道爆炸地面振动的原型试验与数值模拟研究

针对浅埋高压输气管道爆炸产生的地面振动效应,采用现场试验结合数值模拟的方法展开研究。组织实施了全尺寸天然气管道爆炸试验,掌握了高压输气管道爆炸地面振动的量级范围以及衰减规律。经试验数据分析得到,埋地高压天然气管道爆炸造成的地面振动主要产生于物理爆炸过程中,随后发生的天然气爆燃过程并未产生明显的地面振动。基于非线性有限元程序 LS-Dyna建立了高压输气管道爆炸试验计算模型,计算结果与试验现象吻合较好,验证了模型参数设计的合理性。进一步分析了管道爆炸瞬间管内气体-管壁-土体的相互作用机理、应力分布以及裂纹扩展规律。由计算结果分析得到,管道开裂是由于内部高压气体推动管壁向两侧扩展在裂纹尖端处形成了应力集中,管壁冲击土体的速度可达50 m/s,冲击产生的塑性状态向远处传播逐渐衰减为弹性应力波,即形成了地面振动效应。研究成果揭示了高压气体管道爆炸地面振动的主要成因,可为爆炸事故振动预防提供理论参考和技术支持。     

Visualization of deflagration-to-detonation transitions in a channel with repeated obstacles using a hydrogen–oxygen mixture

The deflagration-to-detonation transition in a 100 mm square cross-section channel was investigated for a highly reactive stoichiometric hydrogen oxygen mixture at 70 kPa. Obstacles of 5 mm width and 5, 10, and 15 mm heights were equally spaced 60 mm apart at the bottom of the channel. The phenomenon was investigated primarily by time-resolved schlieren visualization from two orthogonal directions using a high-speed video camera. The detonation transition occurred over a remarkably short distance within only three or four repeated obstacles. The global flame speed just before the detonation transition was well below the sound speed of the combustion products and did not reach the sound speed of the initial unreacted gas for tests with an obstacle height of 5 and 10 mm. These results indicate that a detonation transition does not always require global flame acceleration beyond the speed of sound for highly reactive combustible mixtures. A possible mechanism for this detonation initiation was the mixing of the unreacted and reacted gas in the vicinity of the flame front convoluted by the vortex present behind each obstacle, and the formation of a hot spot by the shock wave. The final onset of the detonation originated from the unreacted gas pocket, which was surrounded by the obstacle downstream face and the channel wall.