构造活动地区工程构造稳定性研究

在０．６１×１０￣５Ｒｅ６．０１×１０￣５，０．９３Ｈ／Ｄ２．５０（Ｈ为波高，Ｄ为圆柱直径）的范围内实验研究了弹性圆柱在浪流联合作用下的流体载荷。通过测量柱表面压力，得到了脉动升力和阻力系数，并给出了Ｍｏｒｉｓｏｎ公式中的Ｃ＿Ｄ，Ｃ＿Ｍ值随Ｋｃ数的变化关系，实验结果表明：在浪流联合作用下的圆柱体，其流体载荷与雷诺数的变化密切相关，并且圆柱的振动对流体载荷也有影响。     

小波浪高雷诺数时串列圆柱的波动压力

在２４０×１０５≤Ｒｅ≤５４０×１０５，２９４≤Ｋｃ×７８５，２５４×Ｌ／Ｄ×５０２的范围内实验研究了串列圆柱在规则波中迎浪前进时的波动压力、波动升力与波动阻力．实验模型由ＰＶＣ管加工制成，表面光滑．实验结果表明：在波流中，当Ｋｃ数较小而Ｒｅ数较高时，绕串列圆柱的流动与均匀流中的绕流有相似之处；随着Ｋｃ数和Ｒｅ数的增加，串列圆柱的柱间干扰效应会发生改变     

几何非对称桩基结构波浪力和群桩系数实验研究

 本文通过对几何非对称群桩进行的一系列规则波和不规则波实验，对六种不同间距、四种不同角度排列的群桩进行了研究．根据非对称群桩波浪力实验数据对无量纲波浪力经验公式进行了修正．在此基础之上推导了非对称群桩结构的群桩系数．     

非定常圆柱绕流的实验研究

本文采用流场显示方法研究单圆柱在非定常流动中的涡旋脱落规律。实验结果表明：在不同的ＫＣ数（ＫＣ＝Ｕ∞Ｔ／Ｄ）下，非常圆柱绕流的涡旋脱落特性是不相同的，一般随ＫＣ数值的增加，其涡旋脱落对数也增加，但有明显的阶梯性，同时圆柱分离点的周期变化后于流场的变化。     

规则波中圆形承台对桩基波浪力的影响

近海软基条件中跨海桥梁和风电场工程大多采用承台桩基结构.圆形承台波浪力的计算采用基于线性势流理论和特征函数展开的解析方法,桩柱波浪力的计算采用Morison公式,讨论并发展了波浪对圆形承台及其下部桩柱的作用力的工程计算方法.研究了承台的存在对桩基波浪力的影响,针对某典型桩基结构布置形式给出了承台效应系数和群桩系数随相对水深、无量纲承台半径、相对浸深等参数的变化规律.     

波浪与外壁开孔双筒柱群的相互作用

应用速度势的特征函数展开和透空壁内两壁间压力差和流体速度成正比的线性模型，建立 了波浪与外壁开孔同轴双筒桩柱群相互作用的线性解析解. 应用这一模型进行了数值计算， 用以检验孔隙系数对双筒柱上的波浪力和波面高度的影响. 结果表明，外壁孔隙系数的增加 对减小波浪力和柱外波面高度有很大影响.     

流体动力干扰对单排圆柱桩列波浪力的影响

多物体之间的流体动力干扰特性对超大型海洋结构物的设计和研究十分重要用波动源在截面周线上分布的方法，就垂直桩柱间三维流体动力干扰对波浪力的影响进行了系统的研究，桩柱的数目可达１００余根得到了柱间流体动力干扰力学机理的若干新的特性尤应指出的是，当桩柱根数超过某一数量后，桩柱上的受力表现出有规律的连续依赖性当柱数很大时，无论柱数是奇数还是偶数，中间大部分的桩柱都将表现出均匀的受力特征这些特性的发现对其他形式多体结构物流体动力干扰的研究也有重要的借鉴和指导意义     

双圆柱绕流特性的模拟研究

采用格子Boltzmann方法对低雷诺数下气体绕流圆柱的规律进行了研究. 对比计算了双 圆柱在不同圆心距、不同Re数、不同来流速度与双圆柱圆心连线角度的情况下，各个圆柱的 受力大小和曳力系数. 结果表明，若Re数为20, 改变圆柱间距，圆柱间距在1.2d和1.4d 之间时，下游圆柱所受曳力有极小值；双圆柱间距为1.6d时，双圆柱受到总曳力最小；圆 柱间距大于2d时，上游颗粒受到的曳力不再受到下游颗粒的影响. 若圆柱间距 为1.2d, 改变雷诺数，Re数在30和40之间，下游圆柱所受曳力有极小值. 另外， 来流速度角度对圆柱的受力影响很大. 上述规律为低Re数下圆柱绕流的深入研究 与应用打下基础.     

三维波浪-流-串行桩柱相互作用的数值分析

为探讨波浪-流-串行桩柱的相互作用,建立了三维数值模型,采用大涡模拟(LES)方法对湍流进行模拟。研究了波浪-流-串行桩柱相互作用下的拖曳系数,对波浪-流靠近结构时的非线性相互作用引起的拖曳力和涡的变化,以及在结构前后自由面的变化进行了分析,并且与波浪-流与孤立桩柱相互作用的研究进行比较。结果表明:由于桩柱的存在,在波浪-流的传播过程中出现了时间延迟,这就导致了桩柱前后附近自由面水位存在较大的位移差;由于桩柱之间互相干扰,下游桩柱的存在导致上游桩柱附近不能形成非对称的周期性涡脱落,上游桩柱横向拖曳力受到影响最大,顺方的拖曳力也受到明显影响;下游桩柱横向和顺向的拖曳力都受到较大的影响;同时涡的脱落会把其附近的自由面吸入。     

相同雷诺数下串列双圆柱绕流的仿真分析

为研究均匀水流场中串列排布的柱群之间的干涉影响,本文以三维串列双圆柱为例,通过计算流体力学(CFD)软件FLUENT15.0中双方程k-ε模型,分析模拟了双圆柱所受平均阻力、平均升力、后柱周向压力、斯特劳哈尔数等水动力特性。结果表明:在雷诺数为Re=2×10~4的串列双圆柱绕流中,两圆柱中心间距L与圆柱直径D的比值为L/D=4时,后柱受前柱绕流尾流影响大,明显高于单圆柱绕流的平均阻力系数,后柱的周向压力值也随前柱尾流的摆动呈现显著的不对称性;当L/D=8时,前柱绕流尾流对后柱影响逐渐减弱;当L/D=12时,两圆柱之间的相互干扰几乎可以忽略,可以看作是相互独立的单圆柱绕流。最后,计算的斯特劳哈尔数与单圆柱绕流对应的斯特劳哈尔数相近且仿真数值在计算数值范围之内,验证了整个仿真分析的准确性,也进一步说明了双圆柱绕流的柱群的干涉影响。双圆柱间距越大,前、后柱之间的干涉影响越弱。     

The diffraction of a solitary wave by a circular cylinder

This paper contributes to the diffraction of a solitary wave by a cylinder, governed by the Boussinesq eq. The Spectrum Method is used to transform 2·D eqs.into a set of 1·D eqs., which is solved by F. D. M. The example given in the paper shows that this method is both accurate and cost effective.     

Effects of an asymmetrical confined flow on a rectangular cylinder

The effects of an asymmetric confined flow on a cylinder of rectangular cross-section are investigated and discussed. Experiments are performed in a wind tunnel by placing cylinders of different cross-sections at various elevations from the floor of the test-section. The Reynolds number is varied within the range 6×10³–4×10⁴. Forces exciting the cylinder are measured by built-in dynamometers placed inside the cylinder structure. The flow is characterized by mean and fluctuating local velocity components to define the inflow distribution and the ensuing wake region. The mean dimensionless force coefficients are then calculated and analyzed. The frequency analysis of the force components acting on the cylinder provides the dynamic characterization of the loading and of the wake shedding. The experimental results highlight that the presence of the wall strongly influences the system dynamics also when the cylinder is placed at a relatively large elevation from the wall itself. The cylinder aspect ratio governs effects of the wall condition on the force coefficients and the Strouhal number.     

Control of mean and fluctuating forces on a circular cylinder at high Reynolds numbers

A narrow strip is used to control mean and fluctuating forces on a circular cylinder at Reynolds numbers from 2.0 × 10⁴ to 1.0 × 10⁵. The axes of the strip and cylinder are parallel. The control parameters are strip width ratio and strip position characterized by angle of attack and distance from the cylinder. Wind tunnel tests show that the vortex shedding from both sides of the cylinder can be suppressed, and mean drag and fluctuating lift on the cylinder can be reduced if the strip is installed in an effective zone downstream of the cylinder. A phenomenon of mono-side vortex shedding is found. The strip-induced local changes of velocity profiles in the near wake of the cylinder are measured, and the relation between base suction and peak value in the power spectrum of fluctuating lift is studied. The control mechanism is then discussed from different points of view. The project supported by the National Natural Science Foundation of China (10172087 and 10472124). The English text was polished by Yunming Chen.     

Measurements of transverse forces on circular cylinders undergoing vortex-induced vibration

Experiments have been carried out on a circular cylinder, with and without helical strakes, free to respond in a direction transverse to a water flow. The Reynolds number range was between 3×10³ and 2.1×10⁴, the mass ratio was just above 0.8 and the fraction of critical damping was approximately 2×10⁻⁴. Measurements are presented of the response, the transverse fluid force and the phase angle between the response and the force, all as a function of reduced velocity. The straked cylinder is observed to respond over a narrow range of reduced velocity and its maximum amplitude is decreased by just over 60%, compared with a plain cylinder. The familiar phase jump that occurs for a plain cylinder did not occur with the straked one, with the phase close to zero over the entire reduced velocity range where response to vortex shedding occurred.     

Heat transfer and flow around a circular cylinder with tripping-wires

An experimental study was conducted on the heat transfer under the condition of constant heat flux and the flow around a circular cylinder with tripping-wires, which were affixed at ± 65° from the forward stagnation point on the cylinder surface. The testing fluid was air and the Reynolds number Red, based on the cylinder diameter, ranged from 1.2 × 10⁴ to 5.2×10⁴. Especially investigated are the interactions between the heat transfer and the flow in the critical flow state, in relation to the static pressure distribution along the cylinder surface and the mean and turbulent fluctuating velocities in the wake. It is found that the heat transfer from the cylinder to the cross flow is in very close connection with the width of near wake.     

Heat transfer due to a round jet impinging normal to a circular cylinder

An experimental investigations of heat transfer for a stationary isothermal circular cylinder exposed normal to an impinging round air-jet has been reported. The circumferential heat transfer distributions as well as axial Nusselt number is measured. The measurements are taken as a function of the Reynolds number ranging from 3.8 × 10³ to 4 × 10⁴, the cylinder separation distance to the nozzle diameter (z/d) varying from 7 to 30, and the nozzle to cylinder diameter ratio (d/D) changing from 0.06 to 0.14. The output results indicated that the axial and radial distributions of the local heat transfer peaked at the impingement point. The heat transfer rate increases as the values of z decreases, for the same d and Re. The drop-off of the Nusselt number with increasing axial distance or radial angle from the impingement point was more pronounced for smaller z and d. The peripheral and surface average Nusselt numbers were determined by integration. The experimental data was used to produce correlations for both average and stagnation point heat transfer. Received on 4 January 1999     

The aerodynamics of a cylinder submerged in the wake of another

Flow-induced fluctuating lift (C_Lf) and drag (C_Df) forces and Strouhal numbers (St) of a cylinder submerged in the wake of another cylinder are investigated experimentally for Reynolds number (Re)=9.7×10³–6.5×10⁴. The spacing ratio L^⁎ (=L/D) between the cylinders is varied from 1.1 to 4.5, where L is the spacing between the cylinders and D is the cylinder diameter. The results show that C_Lf, C_Df and St are highly sensitive to Re due to change in the inherent nature of the flow structure. How the flow structure is dependent on Re and L^⁎ is presented in a flow structure map. Zdravkovich and Pridden (1977) observed a ‘kink’ in time-mean drag distribution at L^⁎≈2.5 for Re>3.1×10⁴, but not for Re≤3.1×10⁴. The physics is provided here behind the presence and absence of the ‘kink’ that was left unexplained since then.     

A compact numerical algorithm for solving the time‐dependent mild slope equation

The mild slope equation has been widely used to describe combined wave refraction and diffraction. In this study, a new numerical algorithm is developed to solve the time‐dependent mild slope equation in a second‐order hyperbolic form. The numerical algorithm is based on a compact and explicit finite difference method that is second‐order accurate in both time and space. The algorithm has the similar structure to the leap‐frog method but is constructed on three time levels for the second‐order time derivative term. The numerical model has the capability of simulating transient wave motion by correctly predicting the speed of wave energy propagation, which is important for the real‐time forecast of the arrival time of storm waves generated in the far field. The model is validated against analytical solution for wave shoaling and experimental data for combined wave refraction and diffraction over a submerged elliptic shoal on a slope (Coastal Eng. 1982; 6 :255). Lastly, the realistic scale Homma's island (Geophys. Mag. 1950; 21 :199) is studied with the use of various wave periods of T = 720s, T = 120 s, and T = 24 s. These wave periods correspond to long, intermediate, and short waves for the given topography, respectively. Comparisons are made between numerical results and existing analytical solutions in terms of the wave amplification around the island, which serves as the indicator for the potential wave runup. Excellent agreements are obtained. The model runs on a PC (Pentium IV 1.8GHz) and the computer capacity allows the computation of a mesh system up to 3000 × 3000, which is equivalent to about 150 × 150 waves or a large area of 540km × 540km for a wave train with the period of T = 60 s. Copyright 2004 John Wiley & Sons, Ltd.     

Time-averaged topological flow patterns and their influence on vortex shedding of a square cylinder in crossflow at incidence

Flow characteristics around the square cylinder and their influence on the wake properties are studied. Time-averaged flow patterns on the surfaces of square cylinder in a cross-stream at incidence are experimentally probed by surface-oil flow technique and analyzed by flow topology for Reynolds numbers between 3.9×10⁴ and 9.4×10⁴ as the incidence angle changes from 0° to 45°. Vortex shedding characteristics are measured by a single-wire hot-wire anemometer for Reynolds numbers between 5×10³ and 1.2×10⁵. The effects of topological flow patterns on the wake properties then are revealed and discussed. Flows around the square cylinder are identified as three categories: the subcritical, supercritical, and wedge flows according to the prominently different features of the topological flow patterns. The Strouhal number of vortex shedding, turbulence in the wake, and wake width present drastically different behaviors in different characteristic flow regimes. A critical incidence angle of 15° separates the subcritical and supercritical regimes. At the critical incidence angle the wake width and shear-layer turbulence present minimum values. The minimum wake width appearing at the critical incidence angle, which leads to the maximum Strouhal number, is due to the reattachment of one of the separated boundary layer to the lateral face of the square cylinder. If the Strouhal numbers are calculated based on the wake width instead of the cross-stream projection width of cylinder, the data in the subcritical and supercritical regimes are well correlated into two groups, which would approach constants at high Reynolds numbers.