多喷口高效能厚翼的研究

提出了以下高效能翼型的思想：用多喷口小速度切向吹气控制厚翼上的流动分离,使流动接近于理想流状况,以产生大升力,小阻力;因多喷口小速度吹气耗能小,故翼型的有效升阻比可以很大．基于雷诺平均N－S方程进行了数值模拟实验．主要结果表明：对于厚度为0.4的儒氏翼型,在升力系数高达3．5时,有效升阻比可达约50（单喷口吹气约为23）;对于厚度为0．4的"升力体"翼型,在升力系数达2．2时,有效升阻比可达40（喷口吹气约为10）．     

基于CFD方法的高墩大跨箱梁桥静风力系数参数影响研究

基于计算流体力学(CFD)对某连续刚构桥主梁不同截面、不同工况下的风场特征进行了数值仿真分析,研究了梁高、风攻角、桥梁横坡等参数对桥梁主梁截面静力三分力系数(阻力系数、升力系数、扭矩系数)的影响,并结合气动流场特征分析了不同截面及攻角下的压强和速度分布。研究结果表明:梁截面高度、风攻角、截面横坡均对桥梁静力三分力系数有较大影响,但三者对三分力系数影响的侧重点不同:梁截面高度对阻力系数影响最大,变化幅度达0.494;攻角对升力系数影响最大,变化幅度达0.382;截面横坡主要体现对阻力系数的影响,变化幅度为0.17。静力三分力系数对梁体截面的形状及尺寸变化较敏感,梁体截面左右侧迎风时,阻力系数相差0.04~0.21,升力系数相差0.009~0.2,扭矩系数相差0~0.07;梁高越大,截面钝体特征越明显,周围的流场分布越复杂。     

门字型输电塔风振响应分析及风振系数的确定

门字型塔是一种综合性能比较好的钻越塔,风荷载对这种高柔结构的影响很大,但实际设计中风振系数按规范统一取值不是很合理,且取值较大,偏于保守。故本文针对门字型输电塔在脉动风作用下的响应、风振系数的求法及合理取值进行专门研究。主要建立了门字型塔ANSYS有限元模型,进行了模态分析;以Davenport风速谱为脉动风功率自谱,应用AR法编制程序顺风模拟了风荷载时程曲线,将由模拟风计算出的风载加载至门字型塔各塔段上对其进行动力时程分析,计算了风振系数并与高耸结构设计规范值进行了比较。研究结果表明:在风载作用下,塔身和横担均会产生较为明显的动力响应;塔身、横担风振系数可取均值,分别为1.39、1.59;规范计算得到的风振系数和本文时程分析得到的风振系数变化规律基本接近,但规范取值较大。     

并列双方柱绕流的Lattice Boltzmann模拟分析

采用Lattice Boltzmann方法对并列双方柱绕流问题进行数值模拟.对方柱间距比s/D=0.2、0.3、0.4、0.5、1.0、1.4、1.5、1.6、1.8、2.0、2.5共11种情况下的流场分别进行计算,给出了对应的流线图、方柱的升力图及阻力图,同时计算了方柱各边中点的压力,给出了压力与间距比的变化曲线,并对各个流线图、升力图、阻力图及压力图进行了分析讨论.结果表明:当s/D≤1.5时,流动呈偏流型,形成周期漩涡;当s/D＞1.5时,流动呈对称型,形成对称漩涡;s/D=1.5为流动从偏流型向对称型转换的临界间距比.该结果对工程中建筑物位置的安排及其安全系数的提高有一定的参考价值.     

固定转捩实验中粗糙带破损对翼型气动特性的影响研究

本文以RAE2822翼型前缘7%位置3mm宽的金刚砂粗糙带为例,研究了粗糙带破损对翼型压力分布的影响。实验结果表明：粗糙带破损会引起激波位置小幅移动,而对翼型后缘压力分布影响很小。当Ma=0.5时,粗糙带破损对升力系数的影响很小;在α≥4°以后粗糙带破损对阻力系数和俯仰力矩系数的影响逐渐增大,且破损位置距翼型中心对称面越远,影响越小。当Ma=0.75时,粗糙带破损对升力系数与阻力系数的影响直到α≥4°后开始逐渐增大,并且随着破损位置远离中心对称面而减弱;俯仰力矩系数对粗糙带破损较为敏感,且粗糙带破损的位置距离中心对称面越远、尺寸越小则影响越小。     

动网格模拟风振对超大瘦高型冷却塔风荷载的影响

利用Fluent软件对超大瘦高型冷却塔的风荷载进行了CFD数值模拟,获得冷却塔外表面的三维流场特性和风压系数分布曲线,并与规范数据进行比较,以验证数值模拟的准确性;利用CFD动网格研究风振条件下冷却塔内外壁的风压分布。结果表明:考虑风振特性后,冷却塔外壁风压呈现增大的趋势,最大负压位置即流动分离点在考虑风振时产生了滞后;对于本文研究的上下开口结构而言,在考虑风振作用后内部风压系数的绝对值整体偏大,且内部高压区的位置发生了变化;不考虑风振时内部风压高压区发生在接近塔底的区域,而考虑风振特性后,内部风压高压区发生在接近塔顶的区域。这说明风振在一定程度上改变了冷却塔内部风压的分布。     

弹性振动对翼型气动特性影响的数值模拟

通过求解雷诺平均非定常Navier-Stokes方程,采用数值模拟方法计算了俯仰和沉浮振动对NACA0012翼型平均气动特性的影响.结果表明:对于俯仰运动而言,在迎角13α≤时的升力°和力矩曲线的线性段部分,振幅角的变化对动态平均升力系数和动态平均力矩系数的影响不明显,与静态时的情况基本一致;当迎角14α≥时,翼型振动的平均升力系数和动态平均力矩系数小°于静态时的情况.同一迎角条件下的俯仰振动频率越高时,其动态的平均升力系数和动态平均力矩系数越大,频率较高时的失速迎角相对于频率较低时的情况有所推迟,但相对于静态的失速迎角而言,不同频率下的动态失速迎角均提前.对于沉浮运动而言,动态平均升力系数随振幅和频率的增加而减小,动态失速迎角随振幅和频率的增大而提前.     

基于实验设计方法的高超声速飞机前缘型线优化分析

为探索前缘线变化对吸气式高超声速飞机气动性能的影响,基于一种旁侧进气布局翼身融合体构型,在飞行马赫数6,攻角4°和高度26 km的巡航飞行条件下,结合运用增量修正参数化设计方法、均匀实验设计方法和计算流体力学模拟,分析了飞行器前缘型线与其升阻力系数及纵向压心等性能参数间的关系.计算结果表明,前缘线形状对飞行器升阻力系数明显高于其对纵向压心影响,设计空间范围内升力系数变化约21.3%,阻力系数变化约31.8%,升阻比变化范围约10.63%,但相对压心变化范围仅为3.87%.在此基础上,通过对典型构型物面压力分布进行分析,发现前缘线形状适当弯曲可利用飞行器下表面侧壁压缩产生的高压气流,利用二者的耦合效应使飞行器获得额外的升力增量.      

带空泡航行体附加质量的数值研究

基于雷诺平均N-S方程和均匀平衡流多相流模型对带半圆球空化器的航行体进行数值模拟,通过捕捉升力曲线来计算不同空化数下的附加质量λ22.研究发现航行体的空泡长度随着空化数的增加而减小,其附加质量系数λ22随着空泡长度的增加而增加,变化关系可以根据空泡长度分为三段.此外,对于做摇荡运动的航行体,升力系数的振荡幅值与附加质量λ22的变化呈正相关关系;同时,响应相对于激励具有滞后效应,并在小空化数时对λ22的计算结果产生较大影响.     

昆虫飞行的高升力机理

对近年来关于昆虫产生非定常高升力的研究进行了综述和归纳.这方面的工作对生物学研究和微型飞行器等微型机械的仿生设计有重要意义.研究表明:果蝇等昆虫翅膀的拍动运动可产生很大的非定常升力,其平均值是定常值的2~3倍,足够平衡昆虫的重量,并有较大的富余用于机动飞行;产生高升力有三个因素:一是拍动开始阶段翅的快速加速运动,二是拍动中的不失速机制,三是拍动结束阶段翅的快速上仰运动.人们从能耗的角度考察了这些非定常高升力机制的正确性和可行性.当作悬停飞行的果蝇用以上机制产生平衡其重量的升力时,其比功率(支持单位身体质量所需的功率)约为29W/kg, 生化/机械效率约为17%. 这些值与人们基于对昆虫肌肉力学特性的研究所预估的值接近.果蝇前飞时,其比功率随速度变化的曲线是一J形曲线,而不是象飞机或鸟的那样是一U形曲线;这与人们基于昆虫新陈代谢率的测量数据所推断的结果一致.对于蜻蜒等(功能上)有前、后两对翅膀的昆虫,有以下初步结果:翅的下拍主要产生升力,上挥主要产生推力;下拍时的平均升力系数可达2~3,十分大,上挥时的平均推力系数可达1~2, 也很大,它们主要由非定常效应产生;前、后翅的相互干扰并未起增大升力和推力的作用,反而有一定的不利作用.      

EXPERIMENTAL DETERMINATION OF THE AERODYNAMIC ADMITTANCE OF A BRIDGE DECK SEGMENT

The gust loading on bridge decks is described by the dynamic forces on a chord-wise strip and by the spatial distribution of these forces across the span. An experimental method to evaluate the aerodynamic admittance of a segment of a bridge deck that includes a combination of the cross-sectional admittance and the spatial distribution of the forces is presented in this paper. The method is based on wind tunnel tests in turbulent flow on a motionless section model of the deck. The approach has been validated experimentally on a closed-box girder bridge deck but can be applied to bridge decks of any cross-section.     

A numerical investigation into the aerodynamic characteristics and aeroelastic stability of a footbridge

The results of a numerical investigation into the aerodynamic characteristics and aeroelastic stability of a proposed footbridge across a highway in the north of England are presented. The longer than usual span, along with the unusual nature of the pedestrian barriers, indicated that the deck configuration was likely to be beyond the reliable limits of the British design code BD 49/01. The calculations were performed using the discrete vortex method, DIVEX, developed at the Universities of Glasgow and Strathclyde. DIVEX has been successfully validated on a wide range of problems, including the aeroelastic response of bridge deck sections. In particular, the investigation focussed on the effects of non-standard pedestrian barriers on the structural integrity of the bridge. The proposed deck configuration incorporated a barrier comprised of angled flat plates, and the bridge was found to be unstable at low wind speeds, with the plates having a strong turning effect on the flow at the leading edge of the deck. These effects are highlighted in both a static and dynamic analysis of the bridge deck, along with modifications to the design that aim to improve the aeroelastic stability of the deck. Proper orthogonal decomposition (POD) was also used to investigate the unsteady pressure field on the upper surface of the static bridge deck. The results of the flutter investigation and the POD analysis highlight the strong influence of the pedestrian barriers on the overall aerodynamic characteristics and aeroelastic stability of the bridge.     

桥面槽缝对桥梁断面静态压力分布影响的实验研究

大跨度斜拉桥或悬索桥的桥梁主梁断面的气动外形是桥梁设计者们很关心的问题之一。对主梁节段模型气动力的风洞实验研究一般都只考虑了来流攻角以及模型本身结构外形的影响，而现今不少大桥在双向来回车道的中间开有槽缝，工程上可以用来改善桥面的空气动力特性以及桥梁本身的稳定性，对于这方面的实验研究进行得不多。本文拟通过风洞实验对某大桥桥梁主梁断面在各种开槽情况下的静态压力分布进行研究，进而对断面各测点的压力分布进行矢量求和获得升力系数、阻力系数和升力矩系数，由此来研究开槽与否以及开槽大小对该桥梁主梁断面的气动力的影响，同时也研究了槽中央隔板的存在对气动力系数的影响。研究表明，隔板的有无对气动力并无明显的影响，而开槽与否以及槽宽的大小对压力分布、升阻力系数以及升力矩系数有明显的影响。     

On the aeroelastic transient behaviour of a streamlined bridge deck section in a wind tunnel

The study deals with the transient behaviour of a two degrees of freedom bridge deck section in a wind tunnel under the effect of an initial excitation. Response of the bridge deck section subjected to an initial mechanical excitation and excitation by an upstream gust is investigated separately. Experiments are conducted with three different frequency ratios between the plunge and pitch degrees of freedom. This experimental study shows that transient growth of energy occurs for wind velocities below the onset of flutter, reaching a level higher than 5 times the level of the initial excitation. In high wind conditions, this means that statistical or spectral computation techniques might underestimate the motion amplitude reached by a flexible bridge deck. This emphasises the importance of using temporal techniques under such circumstances.     

Coupling vibration of vehicle-bridge system

By applying the sinusoidal wave mode to simulate the rugged surface of bridge deck, accounting for vehicle-bridge interaction and using Euler-Bernoulli beam theory, a coupling vibration model of vehicle-bridge system was developed. The model was solved by mode analyzing method and Runge-Kutta method, and the dynamic response and the resonance curve of the bridge were obtained. It is found that there are two resonance regions, one represents the main resonance while the other the minor resonance, in the resonance curve. The influence due to the rugged surface, the vibration mode of bridge, and the interaction between vehicle and bridge on vibration of the system were discussed. Numerical results show that the influence due to these parameters is so significant that the effect of roughness of the bridge deck and the mode shape of the bridge can‘ t be ignored and the vehicle velocity should be kept away from the critical speed of the vehicle_     

基于智能驾驶电动汽车的多车?桥梁耦合系统动力学特性研究

迫于能源和环保问题的压力, 电动汽车及智能驾驶受到了各国高度重视. 轮毂电机驱动电动汽车车轮振动剧烈, 与桥梁路面动力学相互作用更加突出, 现有研究主要针对传统汽车, 关于电动车轮与公路桥梁接触动力学相互作用及智能驾驶车队的多车?桥梁耦合作用研究尚不多见. 本文以轮毂电机驱动电动汽车为研究对象, 考虑车轮和桥面多点接触关系, 研究了两个智能驾驶汽车过桥时的车桥耦合动力学特性. 分析了电机质量、电机激励、轮胎悬架刚度非线性、车距、车速对系统振动特性的影响, 以及桥面不平顺激励、三重耦合激励对电动汽车平顺性的影响. 研究表明: 车距和车速是影响车?桥系统振动特性的重要因素, 在车?桥耦合动态设计中, 车距和车速的影响应重点关注; 桥面越平坦, 电机激励及桥面二次激励对车辆平顺性和道路友好性影响越加显著, 当汽车行驶在平坦桥面时两种激励对轮毂电机驱动电动汽车的影响不容忽视. 所建模型有望为智能驾驶电动汽车与桥梁的耦合作用研究提供理论参考.      

车辆各轮相干桥面不平顺激励的车桥耦合振动

根据车辆左右轮的互功率谱密度和相干函数,推导了左右轮桥面不平顺特性中对应相位角的相干关系,提出了采用相位角相干生成车辆各轮相干桥面不平顺激励的方法,并通过数值算例验证了该生成方法的可靠性.工程应用结果表明,车辆各轮相干桥面不平顺激励增大了桥梁、车辆竖向和车辆俯仰角的振动响应,但降低了车辆侧倾角的振动响应;不同相干函数模...     

An accurate singularity-free geometrically exact beam formulation using Euler parameters

Wind-induced nonlinear oscillations of twin-box girder bridges are very sensitive to the aerodynamic shape of the deck (i.e., slot width ratio (SWR) and wind fairing shape) due to the complicated flow characteristics around the bridge deck. This paper presents a fully integrated finite element (FE) model in time domain, involving a nonlinear aerodynamic force model and a bridge FE model, to allow the investigation of nonlinear oscillation behaviors of long-span twin-box girder bridges with various SWRs and wind fairing shapes. The parameters in integrated FE model were firstly identified by using CFD simulation, and then, the proposed model was validated by conducting wind tunnel testing using sectional models and full-bridge aeroelastic models. It demonstrates that the developed integrated model has the capability of simulating the nonlinear flutter behaviors of twin-box girder bridges with various aerodynamic shapes. Furthermore, the prediction results show that the wind fairing shape has significant impact on the degree of freedom participation in coupled oscillation and failure modes, as well as flutter performance of the bridges. In addition, there is an increase in amplitudes of the limit cycle oscillations with the increase in the SWR of the twin-box girder bridges, and the relationships between the bending-torsional coupled oscillation, failure modes, and SWR of the bridges with anti-symmetric wind fairings are opposite to those with symmetric wind fairings.     

主动控制翼板抑制悬索桥颤振的研究

主动控制翼板是一种新型桥梁气动措施。本文基于非定常气动力理论，推演了安装主动控制翼板后作用在整个桥梁主梁单位长度上气动力表达式，从增加系统扭转阻尼的角度，研究了翼板主动扭转振动参数的选取。在此基础上，对某大跨悬索桥方案进行了二自由度颤振分析，结果表明：合理选取翼板的主动扭转振动参数，主动控制翼板能够有效地提高该桥的颤振稳定性。