隧道洞口段非均质及各向异性土质裂缝仰坡稳定性上限解

针对忽略岩土体非均质和各向异性将导致边坡稳定性评价产生误差的问题,应用极限分析上限理论及抗剪强度系数折减法,推导土体强度非均质和各向异性影响下隧道洞口含裂缝仰坡稳定性解析式,探究土体强度非均质和各向异性对仰坡稳定性系数、坡顶裂缝位置、隧道拱顶失稳范围及仰坡安全系数的影响。结果表明,裂缝深度及坡角越大,仰坡稳定性系数越小;非均质系数越大和各向异性系数越小,维持仰坡稳定的临界坡高越大;非均质系数及各向异性系数越大,裂缝距坡顶边缘越远,隧道拱顶失稳范围越大;非均质系数增大有利于仰坡稳定,而各向异性系数越大仰坡越易失稳。     

Synthesis and Crystal Structure of KCuGd2S4: A Threedimensional Framework with Isolated Channels

The reaction of K₂S₅, Cu, Gd, and S in a 2 : 1 : 2 : 4 molar ratio at 450 °C yields yellow-orange needle-like cuboids of the new quaternary compound KCuGd₂S₄. The crystal structure represents a novel three-dimensional structure type of quaternary rare earth chalcogenides with alkali metal. The compound crystallizes in the orthorhombic space group Cmcm (No. 63) with a = 3.9921(1) Å, b = 13.523(3) Å, c = 13.802(3) Å, V = 745.1(3) ų, Z = 4. In the structure GdS₆ octahedra and CuS₄ tetrahedra are joined by common edges and corners forming corrugated layers parallel to (010). The GdS₆ octahedra are connected via common edges in the third dimension thus leading to the formation of a three-dimensional tunnel structure. The potassium cations are confined within the pentagonal shaped channels and are surrounded by eight sulfide anions each.     

Solution of Wheeler-De Witt Equation, Potential Well and Tunnel Effect

This paper uses the relation of the cosmic scale factor and scalar field to solve Wheeler-De Witt equation,gives the tunnel effect of the cosmic scale factor a and quantum potential well of scalar field, and makes it fit with the physics of cosmic quantum birth. By solving Wheeler-De Witt equation we achieve a general probability distribution of the cosmic birth, and give the analysis of cosmic quantum birth.     

Charge Reconfiguration in Isolated Quantum Dot Arrays

A high level of tunability and control over arrays of quantum dots are key ingredients toward the goal of scalable‐based qubit architectures. Increasing array size simultaneously increases the parameter space and therefore the tuning complexity. The electron reconfiguration behavior of quantum dot arrays isolated from the electron reservoirs is studied experimentally. Isolating a quantum dot array from the reservoirs does not only enable a high degree of control over the tunnel couplings but at the same time drastically simplifies the stability diagrams for small numbers of electrons trapped in the array. Experimental results on double, triple, and quadruple quantum dot arrays are presented and complementary model calculations allow the identification of all transitions observed in the experiment. Highly tunable long‐range transitions are observed in isolated triple quantum dots and evidence of higher‐order cotunneling is found for the quadruple quantum dot array.     

货运动车组装载门凹陷对隧道内会车压力波的影响

随着我国技术经济水平的提高,电子商务产业快速发展,货运动车组应运而生。采用有限体积方法和重叠网格方法,以及SST k-ω高雷诺数湍流模型,数值模拟研究时速350 km的货运动车组在隧道内交会的压力波,探究货运动车组车体结构即装载门凹陷对隧道内交会压力波的影响。实车试验结果验证了本文数值模拟方法的准确性。研究结果表明,凹陷的装载门使平直车身处的最大正压值增大约20%~30%,且有无凹陷的装载门中心最大正压值的差异百分比维持在35%~80%,最大负压值差异百分比在20%~25%。     

高超声速飞行器气动热关联换算方法研究

气动热风洞实验是地面研究和预测飞行器气动热环境的重要手段之一, 但由于风洞实验模拟能力的限制, 风洞实验的流场参数和模型的几何尺度都会与实际飞行情况存在一定的差别, 导致地面风洞实验中得到的模型表面气动加热率数据无法直接用于飞行条件下的热环境预测和热防护设计. 以往通过针对具体飞行器的试验结果进行数据拟合后外插的气动热关联换算方法指向性较强, 没有考虑到气动热的具体影响参数, 存在一定局限性, 难以外推应用于其他外形的飞行器. 为解决通过气动热风洞实验数据外推预测飞行条件下气动热的技术难题, 基于无量纲NS方程和边界层理论分析研究了影响气动热的主要参数, 并通过推导化简边界层近似解热流公式, 针对层流流态建立了气动热关联换算方法, 可以考虑当地边界层外缘参数的影响, 具有一定通用性. 在此基础上, 利用建立的方法将Reentry-F飞行器缩比模型的风洞实验数据换算到该飞行器飞行条件下的典型工况, 并与飞行测量结果进行了比较, 外推预测结果与飞行测量结果符合较好, 表明建立的关联方法可以用于气动热风洞实验数据的外推换算.      

DYNAMIC RESPONSE OF HIGH SPEED TRAIN MEETING IN OPEN AIR,MEETING IN TUNNEL AND PASSING TUNNEL1)

明线会车、隧道会车和过隧道工况下的气动压力波对高速列车的动力响应和运行安全产生很大影响,本文建立了三辆编组的高速列车动力学模型,通过数值仿真得到了列车在三种工况下的车体所受的气动力,基于数值积分分析了列车的动力响应和脱轨系数。研究发现：明线会车和隧道会车工况相比,车辆的侧向运动相反。 明线会车和过隧道时,气动载荷对列车的脱轨系数影响较小,而隧道会车时,气动载荷作用对尾车的安全性影响较大。     

Assessment of Digital Image Correlation as a method of obtaining deformations of a structure under fluid load

Digital Image Correlation (DIC) is employed for the measurement of full-field deformation during fluid–structure interaction experiments in a wind tunnel. The methodology developed for the wind tunnel environment is quantitatively assessed. The static deformation error of the system is shown to be less than 0.8% when applied to a curved aerofoil specimen moved through known displacements using a micrometre. Enclosed camera fairings were shown to be required to minimise error due to wind induced camera vibration under aerodynamic loading. The methodology was demonstrated using a high performance curved foil, from a NACRA F20 sailing catamaran, tested within the University of Southampton RJ Mitchell, 3.5 mx2.4 m, wind tunnel. The aerodynamic forces induced in the wind tunnel are relatively small, compared with typical hydrodynamic loading, resulting in small deformations. The coupled deflection and blade twist is evaluated over the tip region (80–100% Span, measured from the root) for a range of wind speeds and angles of attack. Steady deformations at low angles of attack were shown to be well captured however unsteady deformations at higher angles of attack were observed as an increase in variability due to hardware limitations in the current DIC system. It is concluded that higher DIC sample rates are required to assess unsteady deformations in the future. The full field deformation data reveals limited blade twist for low angles of attack, below the stall angle. For larger angles, however, there is a tendency to reduce the effective angle of attack at the tip of the structure, combined with an unsteady structural response. This capability highlights the benefits of the presented methodology over fixed-point measurements as the three dimensional foil deflections can be assessed over a large tip region. In addition, the methodology demonstrates that very small deformations and twist angles can be resolved.     

基于流固耦合的锚索涡激振动抑制方法研究

悬浮隧道锚索的涡激振动会加剧锚索的疲劳破坏,进而影响悬浮隧道的使用寿命和安全.文章在海洋立管涡激振动抑制研究的基础上,考虑悬浮隧道锚索倾斜角度和来流方向的影响,采用流固耦合的数值方法,对整流罩方法和三控制杆方法的抑制效果进行了分析.结果表明,在顺来流方向,两种方法均具有良好的抑振效果;锚索有倾斜的情况下,三控制杆方法的效果会有所提升;但在来流方向改变时,整流罩方法具有较强的适应性.     

双目视觉技术在高超声速颤振风洞试验中的应用

以验证高超声速颤振风洞试验技术为目标,为了获取试验模型在风洞流场激励下的位移形貌,运用风洞试验的方法研究了某翼面模型的颤振特性。采用一种基于双目视觉系统的试验方法,系统主要由CCD相机、图像采集卡和控制计算机组成,通过立体视觉标定和数字图像处理技术解算出模型变形的形貌。试验结果表明,该方法应用成功,与CFD/CSD数值计算结果比对良好,验证了该技术在高超声速风洞试验中应用的可行性。