共查询到18条相似文献,搜索用时 140 毫秒
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目的观察局部狭窄远心端的流场分布,以便探讨动脉粥样硬化好发区的流场特征。方法数值模拟局部狭窄远心端流场以及剪切应力的分布,粒子图象速度场仪(PIV)测定局部狭窄远心端流场分布。结果数值模拟结果表明局部狭窄远心端流场紊乱,有明显的涡流和二次流形成,并且形成局部的低剪切应力区域,PIV测定的结果证实局部狭窄远心端流场紊乱。结论局部狭窄远心端的流场分布及其特征有利于动脉粥样硬化病变的形成和发展。 相似文献
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采用流体模拟软件,对乳化喷嘴在300 MPa下以水为介质进行模拟分析,得到了引流区、碰撞区、射流区的速度、剪切应力和湍动能分布规律图.模拟结果揭示了3个区域流体流动的基本特征;阐明了每个区域的主要细化机理.对模拟结果进行了理论分析,得出模拟结果和理论分析具有一致性,为喷嘴结构的设计提供了理论依据. 相似文献
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在考虑流体和多孔介质之间瞬时局部非热平衡的前提下,对流体强迫层流横掠多孔介质中等温平板的二维流动应用Brinkman-Forchheime-extended Darcy 模型建立守恒方程组。对方程组进行数量级分析简化,应用积分法进行近似计算,得出了速度边界层厚度、热边界层厚度、壁面黏性摩擦系数和对流传热系数的计算公式。结果表明:在多孔介质中沿平板的速度边界层厚度与光板时明显不同,在平板前端迅速增长,随后逐渐变得平坦,趋于一个恒定值;而热边界层厚度则与光板时类似。 相似文献
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建立了化学气相冷凝反应器内层流状况下流体流动的数学模型,采用SIMPLEC算法求解了反应器内速度和压力的分布,并对计算值和文献值进行了比较。考察了Reynolds准数、直管出口与撞击面的距离等参数对反应器内流型、轴向中心速度、径向最大速度、沿撞击板压力分布的影响规律。 相似文献
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目的 探索计算流体力学(computational fluid dynamics,CFD)技术模拟机械通气状态下呼吸系统内部气流流动的可行性,为CFD技术应用于机械通气的气流流场模拟奠定基础。方法 选取1名健康的中年男性志愿者进行头颈部加胸部MRI扫描,将获得的图像保存为DICOM格式导入Mimics17.0医学图像软件中构建气道三维模型,用Geomagic Studio 12软件进行网格划分后导入Ansys 14.5软件进行CFD模拟计算,对机械通气气道内部气流流场变化进行动态分析。结果 基于MRI图像数据构建气道三维模型,划分网格后对CFD模拟施加不同流速的入口边界条件,分析流速分布、壁压力分布、流场线变化情况以及局部管壁剪切应力的变化情况。结论 基于影像数据对气道进行三维重建,通过对模型进行CFD模拟发现,入口流速与气道内流体流速分布、壁剪切应力及壁压力均呈正相关,入口高流速易在气道分叉处形成涡流。 相似文献
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Deng You-bin Wang Xin-fang Wang Jia-en Li Zhi-an Takahiro Shiota David J. Sahn 《华中科技大学学报(医学英德文版)》1993,13(3):143-150
Summary Nyquist velocity and transorifice pressure gradient dramatically influence color aliasing shape and accuracy of simple hemispherical
flow convergence equation for calculation of flow rate. The present in vitro study was performed to determine whether the
value of Nyquist velocity, at which the shape of proximal isovelocity surface is best fit for a given shape assumption in
different orifice size, and the flow rate may be a determinable and orifice size independent function of clinically measurable
peak velocity or transorifice pressure gradient. Steady flow was driven through circular discrete orifices with diameter of
3. 8 mm, 5.5 mm and 10 mm and flow rate ranging from 2.88 L/min to 8.2 8 L/min. For every flow rate, Doppler color encoded
M-mode images through the center of flow convergence region were transferred into the microcomputer in their original digital
format. The continuous wave Doppler traces of maximal velocity through the orifice were performed for the calculation of pressure
gradient. Direct numerical spatial velocity measure using color pixel intensity was obtained from the transferred color encoded
M-mode images with computer software. The shape of isovelocity surface was determined by the ratio of calculated flow rate
with hemispherical flow convergence equation to the actual flow rate. Both the flow rate and orifice size influence the position
of the velocity profile curve. The shape of isovelocity surface is not constant and changes with the velocities used for the
calculation of flow rates for a given flow rate and orifice size or pressure gradient and also changes with the flow rate
or transorifice pressure gradients for a constant Nyquist velocity and orifice size. It was found that for a given ratio of
calculated flow rate to actual flow rate (0. 7 and 1) the velocities used for the calculation of flow rate with hemispherical
flow convergence equation were correlated well with the pressure gradient for a given orifice size and the differences in
velocities among different orifice sizes adjusted for the covariance pressure gradients were not statistically significant
(P = 0.794 for ratio = 0.7 andP = 0.81 for ratio = l). Our present study provides an orifice size independent quantitative method with which to select the
most suitable Nyquist velocity for applying simple hemispherical flow convergence equation according to clinically measurable
pressure gradients ranging from 5.32 kPa to 26.60 kPa, and offers a correcting factor for the hemispherical flow convergence
equation when pressure gradient is less than 5.32 kPa. 相似文献
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为了提高直线电机在高速、高加速工况下的运动精度,需要对直线电机滑台的摩擦特性进行研究。本文通过直线电机实验台研究了加速度和速度对摩擦力的影响。实验结果表明:加速度越大,预滑动阶段结尾处的临界摩擦力也越大;加速度越大,混合润滑区摩擦滞后现象越显著,使得Stribeck曲线出现后移;在高速运动下,黏滞摩擦力并不随速度呈线性变化,黏滞摩擦因子会随着速度增加而逐渐减小。针对这些摩擦特性,提出了考虑加速度影响的Stribeck二元摩擦模型。结合实验数据辨识出了模型参数并通过对比其他工况下的实验数据和模型预测值,验证了Stribeck二元模型的有效性。 相似文献
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利用双头电导探针测定了固阀塔板上密集鼓泡区气泡的运动速度,考察了密集鼓泡区不同轴向高度的气泡速度分布规律及其分形特征,分析了塔板上密集鼓泡区的气泡运动行为。研究结果表明:不同轴向高度处气泡速度沿同方向的分布具有相似性,近塔中心区域气泡速度变化平缓,呈弱双峰分布;塔板上气泡速度分布具有分形特征,分形维数为1.04~1.25,且随轴向高度的增加均先减小后增大;深层鼓泡区内气泡速度分布的分形维数可以较好地表征气泡运动的湍动强度,两者之间存在线性关系,气泡流湍动强度及分形维数与泡沫层高度间存在指数函数关系。 相似文献