首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到20条相似文献,搜索用时 109 毫秒
1.
基于球形空腔膨胀理论,将煤体在高压水射流冲击下的动态力学响应分为破碎区、裂纹区、弹性区,并分析了各区的力学特征,在此基础上得出了高压水射流冲击下煤体的破碎强度(即高压水射流发生破煤现象的最小冲击压力)的计算公式。将理论计算结果与实验和数值模拟进行对比分析,结果表明:煤体在相同力学参数条件下,数值模拟和模型实验得出的高压水射流破煤压力为15~20MPa,本文理论推导得出的煤体破碎强度(最小破煤压力)为17.86MPa,二者误差小于16%。  相似文献   

2.
为构建Zr62.5Nb3Cu14.5Ni14Al6非晶合金在高压、大应变、高应变率状态下的材料模型,采用根据实验数据理论推导和数值模拟对比反馈的方法,对材料的Johnson-Holmquist本构模型(JH-2模型)参数进行了研究:材料的静水压力-体应变关系通过平板冲击实验数据和理论推导得到;无损材料强度与应变、应变率的关系通过轴向压缩实验数据确定;材料损伤参数与破碎材料强度参数的关系通过平板冲击实验数据确定;破碎材料强度参数通过数值模拟与实验结果对比的反馈法得到。将材料模型应用于平板冲击和破片侵彻的数值模拟,通过数值模拟与实验结果对比的方式,验证材料模型的准确性。结果表明,平板冲击实验中,材料的自由面粒子速度曲线与数值模拟结果吻合度较高;破片侵彻实验中,破片对钢靶的侵彻深度、开坑孔径与数值模拟结果的一致性较好,构建的材料模型较准确反映了材料的动态力学特性。  相似文献   

3.
发射药床冲击破碎过程的数值模拟   总被引:2,自引:0,他引:2  
发射装药挤压破碎是导致膛炸的根本因素,发射药床的破碎动力学是发射安全性理论研究的基础之一.以离散元法为基础,模拟了发射药床的自然堆积过程,获得了发射药床的密实堆积构型;将密实构型下的发射药床离散成弹簧-球单元系统,应用Mohr-Coulomb型破坏准则,对发射药床动态压缩模拟试验装置中的发射药粒在动态载荷下的挤压破碎过程进行数值仿真,并对数值计算结果进行后处理,实现了模拟药室中发射药粒挤压破碎过程数值计算的动画显示,再现了发射药床冲击破碎动力学过程,仿真结果与试验结果吻合较好,验证了论文理论与模型的正确性,为进一步研究发射药床的破碎规律提供了重要的理论基础和计算手段.  相似文献   

4.
无限冰介质中爆炸裂纹扩展机理与数值模拟   总被引:1,自引:0,他引:1  
根据冰体力学性能,提出了无限淡水冰介质在爆炸冲击载荷下的压碎区及裂隙区的理论计算方法.利用大型有限元软件ANSYS/LS-DYNA模拟了爆炸载荷下无限区域冰体内裂纹扩展过程,模拟结果与实验结果基本一致,表明采用的损伤断裂模型能够较准确的反映无限冰介质动态力学性能及裂纹成形过程.数值模型可近似计算冰体中裂隙区的半径.数值计算值与理论计算值误差不超过5%,数值模拟结果与实验结果吻合,从而确定了无限区域冰体在-15℃时的基本破坏特征及范围.  相似文献   

5.
液滴在气体介质中剪切破碎的数值模拟研究   总被引:4,自引:0,他引:4  
液滴变形和破碎是燃料抛撒问题的重要过程.本文将VOF方法和标准k-ε湍流模型组合,建立了计算液滴在气流中变形破碎过程的数值方法.数值模拟了相关的实验,计算得到的液滴破碎过程与实验结果符合较好.在此基础上,分析了几个关键参数(Weber数、Ohnesorge数、液气密度比)对液滴破碎过程的影响.计算结果表明,Weber数...  相似文献   

6.
针对球形粒子组成的散体系统,基于离散单元法,将球形粒子离散成弹簧-球单元系统,给出了离散单元的运动方程,建立了离散单元之间的弹性力和接触力的计算模型,并用Mohr -Coulomb型破坏准则判断粒子的破碎。运用上述方法,对圆筒内由脆性材料组成的散体系统在冲击载荷下的挤压破碎过程进行了数值模拟;计算过程中,跟踪散体系统中每个粒子在不同时刻的破碎情况;分析了散体系统冲击破碎过程数值模拟结果的主要影响因素。结果显示:数值模拟过程中需综合考虑计算精度和计算时间之间的平衡;相同的计算条件下,颗粒的初始堆积方式不同,计算得到的散体系统的破碎程度不同。  相似文献   

7.
采用ANSYS/LS-DYNA软件,对钢筋混凝土墙在受到筒状弹体侵彻撞击、钢筋约束力,及壁面摩擦力等综合作用下的力学效应进行了数值模拟,展现了弹体冲击作用下,钢筋混凝土靶体破碎、飞溅成坑、墙体整体滑移和背面层裂等现象,计算结果与试验宏观破坏现象吻合良好,说明材料模型和参数正确,模拟方法可行.  相似文献   

8.
以高压水射流冲击HTPB推进剂的动态加载过程和准静态加载过程在作用压力和持续时间上的巨大差异为基础, 在水锤压力和滞止压力计算的基础上分别进行了点火模式预判, 然后以模型类比和实验方法分析了动态和准静态加载过程的安全性。结果表明, 使用出口压力在300 MPa以内的高压水射流冲击HTPB推进剂装药在动态加载过程中不会有点火起爆危险性, 但使用100M Pa以上的高压水射流冲击HTPB推进剂装药在准静态加载过程中其内部可能会发生温度突跃情况, 这可能会引起热点火、甚至热起爆。  相似文献   

9.
建立了钻杆力学模型,得出钻杆推力、扭矩与煤体应力之间的关系。分析表明:钻屑过程中,煤体应力增大时,钻杆扭矩增大,钻杆推力减小;煤体强度增大时,钻杆扭矩增加,钻杆推力增大。利用新型钻削设备及推力、扭矩测试装置模拟井下条件进行试验,得到了不同轴压、围压下钻杆推力平均值、扭矩平均值与煤体应力之间的变化规律。试验结果表明:相同的钻机设备不变,外界其它因素一定时,对同种煤岩性质的试件进行钻削,钻杆推力与煤体应力为负相关关系;钻杆扭矩与煤体应力为正相关关系。通过测试钻杆推力和扭矩的实验数值,反演出煤体应力的大小,进而可以预测冲击地压的危险性,研究结果可为煤矿动力灾害预测预报提供一定的理论与实验基础。  相似文献   

10.
Fluent环境中近壁面微空泡溃灭的仿真计算   总被引:3,自引:0,他引:3  
基于FLUENT软件环境,采用VOF模型和非稳态方法求解Navier-Stokes方程,模拟了近壁面的空泡溃灭过程,同时计算了空泡溃灭处与壁面的距离对射流强度的影响.结果表明:在近壁面,空泡将形成非对称溃灭,因水锤作用,引发高速水射流在壁面产生高压而形成空蚀破坏;基于FLUENT环境的计算结果与已有的实验和计算结果相符,为研究空泡溃灭和空蚀机制提供了类比的数值计算方法.  相似文献   

11.
 The effects of several influencing parameters on the thickness distribution of a liquid sheet formed by two impinging jets are examined using a simple interferometric method which can provide sharp and clear fringe images in spite of very simple optical setup. The parameters changed in this study are the impinging angle, orifice diameter, liquid jet velocity, and liquid viscosity. The experimental results are compared with existing theoretical predictions. A larger impinging angle, smaller orifice diameter, and a higher azimuthal angle are found to result in thinner liquid sheets, although jet velocity itself does not have any effect on the sheet thickness. Higher viscosity, on the other hand, is found to yield a thicker liquid sheet, which has not been considered in the theoretical analysis so far. The theoretical models used for comparison predict the same trend as the experimental results, but the thickness values are overestimated at low azimuthal angles. This discrepancy is gradually lessened as the azimuthal angle is increased. More refined theoretical modeling that decreases this difference and includes the effect of physical properties of liquid is necessary. Received: 26 May 2000/Accepted: 8 November 2000  相似文献   

12.
The spatially resolved effectiveness distributions for a single jet and row of circular jets impinging on a convex surface are reported in the present study. The impinging surface was inclined at 0°, 15°, 30° and 45° to the jet axis. Studies were conducted for a single curvature ratio equal to 0.05 at a constant Reynolds number equal to 40,000 for non-dimensional jet-to-target distances, L/d equal to 2, 4, 6, 8 and 10. Two non-dimensional jet-to-jet spacings, S/d, equal to 4 and 8 were studied. The effectiveness distribution for multiple jet impingement was noticed to be different from that for a single jet impingement. The entrainment from the surrounding was mitigated for the inner jets by the outer jets. The interaction of adjacent walljets forms a ‘barrier’ against the percolation of entrained ambient from the outer jet region towards the inner region. The zone of walljet interaction and region near to the inner jets were therefore observed to result in high effectiveness values. The inclined impingement of the jet reduces the strength of interaction of the walljets on up and downhill sides and thereby reduces the ‘barrier effect’ against the entrainment of ambient, which causes similar variation of effectiveness for all the jets in a row at high inclinations.  相似文献   

13.
湍流冲击射流流动与传热的数值研究进展   总被引:15,自引:0,他引:15  
陈庆光  徐忠  张永建 《力学进展》2002,32(1):92-108
湍流冲击射流由于其冲击表面时具有很高的局部传热率和冲击 力,被广泛应用于如表面的加热、电子元件的冷却、纸张的干燥和材料 的切割等工程应用和工业过程中.由于其流动的复杂性,也常被作为一 种理想的测试实例来评价湍流模型的性能.此外,湍升力射流与地面之 间的空气动力作用对V/STOL (垂直或短距离起落)飞机的性能具有很大 的影响.长期以来,人们从理论分析、实验测量和数值模拟方面对冲击 射流进行了广泛而系统的研究,积累了丰富的资料.本文在分析了湍流 冲击射流的数值研究现状的基础上,对近年来有关湍流冲击射流流动与 传热的数值研究方面的文献有选择地进行了综述,重点评述了不同湍流 模型对冲击射流流动与传热的预测能力,讨论了存在的问题并对该领域 今后的研究方向进行了展望.  相似文献   

14.
The five-stage cylindrical stepped-wall observation chamber is designed to investigate the method of controlling the interior ballistic stability in bulk-loaded propellant guns. The expansion and mixing process of twin combustion gas jets in liquid is studied by means of high speed photographic system. The influence of multiple parameters on jet expansion shape is discussed. Based on the experiment, the three-dimensional mathematics model is established to simulate the expansion process of twin gas jets in liquid. The pressure, density, temperature, velocity contours and evolutionary process of vortices are obtained. Results show that vortices behind the corner of the steps are formed due to the inducing effect of steps. The jets can expand along the axial and radial direction simultaneously, weakening the Kelvin-Helmholtz instability. The numerical simulation results of axial expansion displacement are in good agreement with the experimental data.  相似文献   

15.
The numerical simulation method to study rock breaking process and mechanism under high pressure water jet was developed with the continuous mechanics and the FEM theory. The rock damage model and the damage-coupling model suited to analyze the whole process of water jet breaking rock were established with continuum damage mechanics and micro damage mechanics. The numerical results show the dynamic response of rock under water jet and the evolvement of hydrodynamic characteristic of jet during rock breaking is close to reality, and indicates that the body of rock damage and breakage under the general continual jet occurs within several milliseconds, the main damage form is tensile damage caused by rock unload and jet impact, and the evolvement of rock damage shows a step-change trend. On the whole, the numerical results can agree with experimental conclusions, which manifest that the analytical method is feasible and can be applied to guide the research and application of jet breaking rock theory.  相似文献   

16.
An experimental study has been made of the rate at which steam condenses on a pool of turbulent water, under conditions where diffusion of heat in the liquid phase is the controlling factor. A variety of flow configurations have been examined, including a vertical jet impinging on the free surface from below, grid turbulence decaying in an open channel and recirculating flows generated by submerged horizontal jets. It was found that the theoretical model proposed by Theofanous, Houze & Brumfield (1976) provided a basis for correlating the results. In addition, the experiments on the vertical jet arrangement supported the prediction of Gardner & Crow (1973) that as agitation increases a condition is reached, characterized by a critical Kutateladze number, beyond which the condensation rate is considerably enhanced.  相似文献   

17.
The rate of heat transfer from a plate due to impinging of an array of jets was investigated. The effect of jet-to-plate spacing in a confined array of impinging laminar square jets was investigated numerically through the solution of Navier Stokes and energy equations. The simulation is carried out for the jet-to-plate spacing between 2 B and 20 B and for jet-to-jet spacing of 4 B, where B is the jet width. Five in-line jets subjected to across-flow were used in this investigation. Also, six different ratios of jet to cross-flow velocity are simulated (0.5, 1.0, 2.5, 5, 7.5 and 10) for the jet Reynolds number of 200. The predicted results show a formation of one or two ground horseshoe vortices between the jets. In addition, a horseshoe vortex forms at different position between the orifice and impinging plates due to the interaction of two jets before they combine. The number of the ground horseshoe vortex and its size are strongly affected by the jet-to-plate spacing and by jet to cross-flow velocity ratio. The effect of jet-to-plate spacing and jet to cross-flow velocity ratio on heat transfer is presented and discussed.  相似文献   

18.
Two-dimensional normal impinging jet flowfields, with or without an upper plate, were analysed by employing an implicit bidiagonal numerical method developed by Lavante and Thompkins Jr. The Jones–Launder K–? two-equation turbulent model was employed to study the turbulent effects of the impinging jet flowfield. The upper plate surface pressure, the ground plane pressure and other physical parameters of the momentum flowfield were calculated at various jet exit height and jet inlet Reynolds numbers. These results were compared with those of Beam and Warming's numerical method, Hsiao and Chuang, and others, along with experimental data. The potential core length of the impinging jet without an upper plate is longer than that of the free jet because of the effects of the ground plane, while the potential core length of the impinging jet with an upper plate is shorter than that of the free jet because of the effects of the upper plate. This phenomenon in the present analysis provides a fundamental numerical study of an impinging jet and a basis for further analysis of impinging jet flowfields on a variable angle plate.  相似文献   

19.
周期激励下单搭接接头强度与振动特性研究   总被引:1,自引:0,他引:1  
主要研究汽车轻量化粘接结构在周期性振动载荷激励下强度与振动属性的改变。首先,利用实验手段,研究了振动载荷对单搭接接头疲劳特性的影响,分析了疲劳后接头的强度及模态频率的变化;其次,通过仿真分析方法,建立了基于经典双线性内聚力模型(Cohesive Zone Model)的单搭接接头静态及动态仿真模型,对胶接接头的模态频率、振型及加载开裂过程中胶层单元失效扩展进行模拟,与此同时,探讨了疲劳载荷对胶层内聚力模型的弱化效应。最后,利用SEM电镜分析手段,从微观上分析了粘接接头疲劳损伤及断裂机理。  相似文献   

20.
Heat transfer from an obliquely impinging circular, air jet to a flat plate   总被引:5,自引:0,他引:5  
A series of experiments was conducted for the measurement of local convective heat transfer coefficients for an obliquely impinging circular air jet to a flat plate. In the experiments, the oblique angles selected were 90°, 75°, 60° and 45°, with 90° being a vertical jet. Two different Reynolds numbers of 10,000 and 23,000 were considered for the purpose of comparison with previous data available in the literature. Another parameter varied in the measurements was the dimensionless jet-to-plate distance, L/D. Four values of L/D(2, 4, 7, and 10) were considered in the experiments. The experiments were conducted using the preheated wall transient liquid-crystal technique. Liquid-crystal color changes were recorded with a video system. Local convective heat transfer coefficients were obtained through the surface transient temperatures that were related to the recorded color information. Detailed local heat transfer coefficients were presented and discussed in relation to the asymmetric wall jet upon impingement of the jet flow. Results of experiments show that, for a given flow situation, the point of maximum heat transfer shifts away from the geometrical impingement point toward the compression side of the wall jet on the axis of symmetry. The shift is more pronounced with a smaller oblique angle (larger jet inclination) and a smaller jet-to-plate distance. Comparisons of experimental results with existing heat transfer data for both obliquely impinging jets and vertical impinging jets are made. The effect of oblique angles on heat transfer was assessed.  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号