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圆柱体BGO探测器时间性能的研究
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作者 叶沿林 周长春 +1 位作者 林俊松 刘昕 《核电子学与探测技术》 CAS CSCD 北大核心 1992年第4期220-224,共5页
实验测得φ40mm×40mmBGO在GDB50L和GDB44D光电倍增管上的时间分辨率为1.9,3.4ns(对^(60)Co),φ76mm×100mmBGO在GDB76F上的时间分辨率为6.3ns。用蒙特卡罗方法研究了光电倍增管对探测器时间性能的影响,预计φ76mm×100mmBG... 实验测得φ40mm×40mmBGO在GDB50L和GDB44D光电倍增管上的时间分辨率为1.9,3.4ns(对^(60)Co),φ76mm×100mmBGO在GDB76F上的时间分辨率为6.3ns。用蒙特卡罗方法研究了光电倍增管对探测器时间性能的影响,预计φ76mm×100mmBGO在3英寸快管上的时间分辨率可在2.5ns以下。 展开更多
关键词 BGO 时间分辨 探测器 圆柱体型
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圆柱体弯曲行波压电超声电机运动机理的研究 被引量:28
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作者 赵向东 刘长青 赵淳生 《应用力学学报》 CAS CSCD 北大核心 2000年第3期120-123,共4页
论述了圆柱体弯曲行波压电超声电机的运动及动力传递机理 ,对其定子进行了有限元模态分析 ,并针对所选用的工作模态详细推导了定子表面质点的椭圆运动轨迹方程 ,为进一步定量分析该型电机的动力的传递及定子尺寸的优化设计提供了理论依据。
关键词 超声电机 工作模态 运动轨迹 圆柱体弯曲行波
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外形变化对圆柱体结构绕流特性的影响
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作者 涂佳黄 张志豪 +2 位作者 王志忠 胡刚 梁经群 《防灾减灾工程学报》 CSCD 北大核心 2021年第5期1071-1079,共9页
基于CFD流体计算平台Fluent计算软件,对雷诺数Re=3900下波浪型圆柱体结构三维绕流问题进行了研究,主要分析波长比(λ/D_(m)=1.8~5.0)与波幅比(a/D_(m)=0.05~0.2)两个关键参数对波浪型圆柱体的绕流特性及其尾流场分布特性的影响且引入了... 基于CFD流体计算平台Fluent计算软件,对雷诺数Re=3900下波浪型圆柱体结构三维绕流问题进行了研究,主要分析波长比(λ/D_(m)=1.8~5.0)与波幅比(a/D_(m)=0.05~0.2)两个关键参数对波浪型圆柱体的绕流特性及其尾流场分布特性的影响且引入了光滑圆柱(UC)计算结果作对比,并进一步揭示其内在的尾流控制机理。研究表明:波浪型圆柱体尾流特性存在强烈的三维效应,节点处与鞍形处流场特性分布存在明显差异;波浪型圆柱尾流区的顺流向时均速度分布呈现出半对称U型,而轴向方向的时均速度分布则呈现出强烈的三维效应;波浪型柱体沿径向方向压力分布也呈现出强烈的三维效应,一般在节点处的压力达到最小值,在中间截面处压力值达到最大;随波幅比增大,阻力系数平均值与脉动性升力系数大致呈现出衰减趋势,并在a/D_(m)=0.2处达到最小值。波浪型柱体结构压差阻力的减少为结构流动控制提供相关支撑。 展开更多
关键词 波浪圆柱体 波长比 波幅比 流体力系数 耦合机理
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Numerical simulation of flow around square cylinder using different low-Reynolds number turbulence models 被引量:3
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作者 张泠 周军莉 +2 位作者 陈晓春 兰丽 张楠 《Journal of Central South University of Technology》 EI 2008年第4期564-568,共5页
ABE-KONDOH-NAGANO,ABID,YANG-SHIH and LAUNDER-SHARMA low-Reynolds number turbulence models were applied to simulating unsteady turbulence flow around a square cylinder in different phases flow field and time-averaged u... ABE-KONDOH-NAGANO,ABID,YANG-SHIH and LAUNDER-SHARMA low-Reynolds number turbulence models were applied to simulating unsteady turbulence flow around a square cylinder in different phases flow field and time-averaged unsteady flow field.Meanwhile,drag and lift coefficients of the four different low-Reynolds number turbulence models were analyzed.The simulated results of YANG-SHIH model are close to the large eddy simulation results and experimental results,and they are significantly better than those of ABE-KONDOH-NAGANO,ABID and LAUNDER-SHARMR models.The modification of the generation of turbulence kinetic energy is the key factor to a successful simulation for YANG-SHIH model,while the correction of the turbulence near the wall has minor influence on the simulation results.For ABE-KONDOH-NAGANO,ABID and LAUNDER-SHARMA models satisfactory simulation results cannot be obtained due to lack of the modification of the generation of turbulence kinetic energy.With the joint force of wall function and the turbulence models with the adoption of corrected swirl stream,flow around a square cylinder can be fully simulated with less grids by the near-wall. 展开更多
关键词 low-Reynolds number turbulence model flow around square cylinder numerical simulation
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Fluid Flow Past a Circular Cylinder with Tandem Rod and Staggered Rod at Low Reynolds Number 被引量:2
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作者 WU Wenbo WANG Jiasong 《Journal of Ocean University of China》 SCIE CAS CSCD 2018年第5期1053-1065,共13页
The flow past a primary cylinder with one tandem control rod and one staggered control rod is simulated in this paper through solving the Navier-Stokes equations. Two examples are simulated to validate the model, and ... The flow past a primary cylinder with one tandem control rod and one staggered control rod is simulated in this paper through solving the Navier-Stokes equations. Two examples are simulated to validate the model, and the results matched well with those of previous researches. The Reynolds number based on the diameter of the primary cylinder is 500. The diameter ratio between the control rod and the primary cylinder (d/D) is 0.25. It was found that the effect of the combination of one upstream tandem control rod and one staggered control rod on the hydrodynamics of the primary cylinder is a linear superposition of the effect of a corresponding single control rod, and the effect of the upstream tandem control rod is dominant at larger spacing ratios such as G/D=2. For the combination of a downstream tandem control rod and a staggered control rod, the effect of the control rods is different from that of the corresponding single control rod in the region of 0.2〈G/D〈0.5 & 30°〈a〈120° and 0.9〈G/D〈1.4 & 30°〈a〈50°, where the additional effect is obvious. In this case, the effect of the downstream tandem control rod is dominant at small spacing ratios (such as G/D=0.1). At moderate spacing ratios such as G/D=0.4, the effects of the tandem control rod and the staggered control rod are comparable in both cases. 展开更多
关键词 tandem and staggered control rods additional effect of double control rods vortex shedding drag and lift coefficients numerical simulation
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