水中开孔腔流激振荡控制实验研究

水中开孔腔流激振荡是水下航行器的一类突出噪声源. 为探究有效抑制水中开孔腔流激振荡的控制方法和作用特性, 首先以水下航行器的表面开孔结构为对象设计了开孔腔模型, 并提出一种基于来流边界层分流原理的流动控制装置——前缘分流体, 借助循环水洞装置对水中开孔腔的流激振荡特性及其控制进行了实验研究. 通过沿流向和展向安装于腔底的动态压力传感器测量腔内脉动压力, 分别从腔内脉动压力的频谱特性和空间分布特性两方面, 探讨了水中开孔腔在不同流速下的流激振荡特性和前缘分流体对水中开孔腔流激振荡的控制效果, 并对前缘分流体的主要作用机理进行了分析. 研究结果表明: 水中开孔腔流激振荡形式以剪切层自持振荡为主, 在流速较低时, 如2.4 m/s, 就会产生稳定的自持振荡, 且具有随流速升高而急剧增大的趋势; 前缘分流体对水中开孔腔绕流自持振荡具有良好的抑制效果, 且抑制效果随流速增加而显著提升, 对腔内脉动压力频谱峰值和总级的最大抑制量分别达到25.3 dB和15.6 dB; 此外, 前缘分流体对开孔腔流激振荡具有低频频移作用, 有益于避免发生流激空腔共振; 脉动压力空间分布特性表明, 前缘分流体对水中开孔腔流激振荡抑制机理主要在于破坏了腔内流场受到的周期调制作用.      

导流板对腔口流体自持振荡影响的研究

腔口流体动力自持振荡的频率和导流板的长度有一定关系。本文通过对跨越腔口非稳定层和自持振荡的理论分析，并通过对不同长度导流板的腔、低速流激自持振荡均方压力谱分析的实验研究，给出流激自持振荡的频率与导流板长度之间的关系。流体动力振荡和腔的声驻波共振耦合时，腔内振荡的均方压力达到最大值。根据流速变化时，均方压力谱峰值频率的偏移，分析了导流板长度对流引起的流一腔系统耦合共振的影响。     

侧加热腔体内重力波演化过程的数值模拟

利用二维数值模拟的方法研究了侧加热腔体内的自然对流．基于数值模拟结果,描述了水平热入侵流(intrusion)的整个演化过程,并对该过程的物理机制进行了讨论．结果表明：当热入侵流抵达腔体冷壁后,由于冷壁无法卷入所有的热入侵流,热入侵流在冷上角堆积并产生一个反向流动,在冷壁边界层附近形成一个顺时针涡,该涡在浮力效应驱动下可返回热壁,并在腔体的冷热壁之间形成了腔体尺度的流体振荡,即内重力波．     

流向振荡圆柱绕流的格子Boltzmann方法模拟

用一种新近发展起来的格子Boltzmann方法(LBM)在相对较小的雷诺数(Re \le 200)条件下模拟了不可压缩的流向振荡圆柱绕流问题, 考查了涡脱落模态和升阻力特性. 通过模拟, 在近尾流区发现了实验研究中已经发现的对称/反对称的涡脱落模态, 包括有些传统数值方法未发现的模态. 研究了频率锁定区域的范围及其与振幅的关系, 发现振幅越大, 发生锁定的频率区域越宽. 此外还对升阻力进行了定量意义的模拟,研究了振荡频率和振幅与升阻力的关系.      

大型离心叶轮振动模态局部化特性研究

为了研究目前工程中大型流体机械离心叶轮出现的局部疲劳破坏的机理,基于现有的有限元分析方法,结合模态分析等动力学理论以及叶轮所承受的气流激励,对其动力学特性进行了研究。着重研究了离心叶轮这类周期循环对称性结构具有的不同于非周期循环结构的特殊动力学性质以及该特殊的动力学特性与叶轮疲劳破坏的联系。研究发现其存在频率通带(passbands)、频率禁带(stopbands)现象,并出现了振动模态局部化现象。另外,叶轮的动力学特性对其周期性结构失谐特别敏感,该类失谐可来自由制造误差、材料和使用中磨损出现的不均匀等多种因素。对于协调结构,在一定条件下(如系统具有高密集模态),很小的失谐量(1%)就可使结构振动模态产生急剧变化,从而出现振动模态局部化现象。对于所研究的机组,当进口预旋器导致的流体激振频率(1166.7Hz)接近叶轮的由第12阶～18阶固有频率组成的禁带(1020.3～1054.5 Hz)时,数值分析结果显示叶片进口部位出现了振幅较大的振动,与该机组实际破坏的部位相符。研究结果表明所使用的振动模态局部化分析方法能够揭示叶轮发生疲劳破坏的原因,即是一类共振型疲劳破坏现象。     

导流板对腔口液体自持振荡影响的研究

腔口流体动力自持振荡的频率和导流板的长度有一定关系。本文通过对跨越腔口非稳定层和自持振荡物理论分析，并通过对不同长导流板的腔、低速流激自持振荡均方压力谱分析和实验研究，给出流自持振荡的频率与导流板长度之间的关系。     

管道液体流速对超声导波纵向模态传播的影响分析

建立了充液管道中液体流动时超声导波纵向模态的群速度频散方程,研究了模态、激励频率对载流管道内超声导波传播的影响。在数值仿真的基础上,利用环形压电阵列在载流管道中激励接收频率305kHz的L(0,5)模态,对纵向模态在载流管道中的传播特性进行了实验研究。研究结果表明,载流管道内频率305kHz的L(0,5)模态的群速度与液体流速呈近似线性变化。实验结果与理论分析结果相符,该结论为载流管道流量在线测量提供了一种新方法,为超声导波流量计的研制打下了理论基础。     

高超声速稀薄流中横向喷流干扰特性实验研究

喷流干扰是高超声速飞行高精度控制的一种有效手段,研究者们以往大部分都主要集中于连续流条件下喷流干扰效应的机理研究,并给出了喷流干扰流场的典型结构,而稀薄流条件下喷流干扰特性的实验数据还十分匮乏.本文利用JFX爆轰激波风洞产生高超声速稀薄自由流,基于平板模型开展不同喷流压力和自由来流参数对横向喷流干扰特性影响的实验研究,采用高速纹影成像及图像处理技术,获得稀薄流条件下喷流干扰流场演化过程及流场结构的变化规律.相比于无喷流条件形成的流场,横向喷流与稀薄自由流相互作用形成的流场结构更为复杂,喷流压力由于受到稀薄来流的扰动,斜激波会短暂穿透喷流干扰流场并延伸至楔形体上部.喷流干扰流场内桶状激波的影响范围随着喷流压力的升高而逐渐变宽,位于三波点上游的斜激波空间位置不会随喷流压力的变化而改变,而位于三波点下游的弓形激波则向上游移动,当喷流压力过低时,桶状激波不会与其他两种激波交汇形成三波点.高超声速稀薄来流压力的降低同样会使桶状激波的影响范围变宽,弓形激波同样也会向上游移动,但基本不会对斜激波空间位置产生任何影响.     

流向强迫振荡圆柱绕流的涡脱落模态分析

通过求解采用ALE方法描述的运动坐标系Navier-Stokes方程组，分析均匀来流下雷诺 数为150的静止和流向振荡的圆柱绕流. 主要研究了强迫振荡频率和较大振幅比 (A/D=0.3-1.2)对圆柱升力、阻力变化特性以及涡脱落模态的影响. 研究表 明，流向振荡圆柱绕流存在多种涡脱落模态，如对称S以及反对称A-I, A-III, A-IV等多种形式；比较研究结果，拓展了各模态下对应的锁定区域，并将其分为5个 子区；A-I模态中圆柱受力较以前所知更复杂；通过分析计算结果，发现最大加速度 比Af_{c}^{2}/Df_{s0}^{2}可能是涡脱落模态(尤其是对称S模态)最有效的控制参数.     

Maxwell流体管内起动流的研究

对Maxwell流体流体管内起动流的振荡特性进行研究，得到了描述振荡特性的解析解。研究了黏弹性参数对各时刻速度剖面的影响，获得了轴心速度，平均速度和壁面摩擦力随时间的变化规律以及它们的频率特征。结果表明振荡的基频成分决定了流动的主要特性，给出了并分析了基频频率与振幅和黏弹性参数之间的关系。     

A calculating method of shock wave oscillating frequency due to turbulent shear layer fluctuations in supersonic flow

One of the more severe fluctuating pressure environments encountered in supersonic orhypersonic flows is the shock wave oscillation driven by interaction of a shock wave withboundary layer.The high intensity oscillating shock wave may induce structure resonanceof a high speed vehicle.The research for the shock oscillation used to adopt empirical orsemiempirical methods because the phenomenon is very complex.In this paper atheoretical solution on shock oscillating frequency due to turbulent shear layer fluctuationshas been obtained from basic conservation equations.Moreover,we have attained theregularity of the frequency of oscillating shock varying with incoming flow Mach numbersM_∞and turning angleθ.The calculating results indicate excellent agreement withmeasurements.This paper has supplied a valuable analytical method to study aeroelasticproblems produced by shock wave oscillation.     

Hydrodynamics of flow over a transversely oscillating circular cylinder beneath a free surface

In this paper, hydrodynamic force coefficients and wake vortex structures of uniform flow over a transversely oscillating circular cylinder beneath a free surface were numerically investigated by an adaptive Cartesian cut-cell/level-set method. At a fixed Reynolds number, 100, a series of simulations covering three Froude numbers, two submergence depths, and three oscillation amplitudes were performed over a wide range of oscillation frequency. Results show that, for a deeply submerged cylinder with sufficiently large oscillation amplitudes, both the lift amplitude jump and the lift phase sharp drop exist, not accompanied by significant changes of vortex shedding timing. The near-cylinder vortex structure changes when the lift amplitude jump occurs. For a cylinder oscillating beneath a free surface, larger oscillation amplitude or submergence depth causes higher time-averaged drag for frequency ratio (=oscillation frequency/natural vortex shedding frequency) greater than 1.25. All near-free-surface cases exhibit negative time-averaged lift the magnitude of which increases with decreasing submergence depth. In contrast to a deeply submerged cylinder, occurrences of beating in the temporal variation of lift are fewer for a cylinder oscillating beneath a free surface, especially for small submergence depth. For the highest Froude number investigated, the lift frequency is locked to the cylinder oscillation frequency for frequency ratios higher than one. The vortex shedding mode tends to be double-row for deep and single-row for shallow submergence. Proximity to the free surface would change or destroy the near-cylinder vortex structure characteristic of deep-submergence cases. The lift amplitude jump is smoother for smaller submergence depth. Similar to deep-submergence cases, the vortex shedding frequency is not necessarily the same as the primary-mode frequency of the lift coefficient. The frequency of the induced free surface wave is exactly the cylinder oscillation frequency. The trends of wave length variation with the Froude number and frequency ratio agree with those predicted by the linear theory of small-amplitude free surface waves.     

Mode transition and oscillation suppression in supersonic cavity flow

Supersonic flows past two-dimensional cavities with/without control are investigated by the direct numerical simulation(DNS). For an uncontrolled cavity, as the thickness of the boundary layer declines, transition of the dominant mode from the steady mode to the Rossiter Ⅱ mode and then to the Rossiter Ⅲ mode is observed due to the change of vortex-corner interactions. Meanwhile, a low frequency mode appears. However, the wake mode observed in a subsonic cavity flow is absent in the current simulation.The oscillation frequencies obtained from a global dynamic mode decomposition(DMD)approach are consistent with the local power spectral density(PSD) analysis. The dominant mode transition is clearly shown by the dynamic modes obtained from the DMD. A passive control technique of substituting the cavity trailing edge with a quarter-circle is studied. As the effective cavity length increases, the dominant mode transition from the Rossiter Ⅱ mode to the Rossiter Ⅲ mode occurs. With the control, the pressure oscillations are reduced significantly. The interaction of the shear layer and the recirculation zone is greatly weakened, combined with weaker shear layer instability, responsible for the suppression of pressure oscillations. Moreover, active control using steady subsonic mass injection upstream of a cavity leading edge can stabilize the flow.     

基于OAET和HHT的混凝土AE源损伤识别方法

针对混凝土材料中所产生的声发射(AE)信号复杂的特点,采用正交异性声发射传感器(OAET)提取结构中特定方向的AE信号。运用Hilbert-Huang变换(HHT)对AE信号进行分析,通过循环应用经验模态分解的方法,将复杂的原始数据序列分解为有限数目的固有模态函数及一个残余项,进而采用Hilbert变换,得到以时间为自变量的信号幅度和瞬时频率函数。文章探讨了基于幅度和瞬时频率函数的损伤识别方法,形成了一种混凝土中复杂AE信号处理及损伤识别的新途径,有助于AE技术的发展与推广应用。     

Oscillation of shallow flow past a cavity: Resonant coupling with a gravity wave

Self-excited oscillations of flow past a cavity are generated in a shallow free-surface system. The shear layer past the cavity opening has two basic forms: a separated free-shear flow; and a shear flow along a slotted plate. Instabilities of these classes of shear flows can couple with the fundamental gravity-wave mode of the adjacent cavity. The dimensionless frequencies of both types of oscillations scale on the length of the cavity opening, rather than the gap distance between the slats, i.e., a large-scale instability is always prevalent. A technique of high-image-density particle image velocimetry allows acquisition and interpretation of global, instantaneous images of the flow pattern, including patterns of vorticity and Reynolds stress correlation. Use of a cinema approach provides representations of the timewise evolution of the global, instantaneous flow structure, and thereby definition of the amplitude peaks and phase angles of the coupled fluctuations via auto- and cross-spectral techniques. These methods, along with global, averaged representations of the fluctuating flow field, provide insight into the onset of fully coupled (phase-locked) oscillations of the shear flow past the resonator cavity. The common, as well as the distinctive, features of the resonant-coupled instability of the shear flow past the slotted plate are characterized, relative to the corresponding coupled instability of the free-shear layer. Varying degrees of resonant coupling between the unstable shear layer and the adjacent resonator are attained by variations of the inflow velocity, which yield changes of the predominant oscillation frequency, relative to the resonant frequency of the adjacent cavity. Well-defined, coherent oscillations are indeed attainable for the case of the shear flow along the slotted plate, though their amplitude is significantly mitigated relative to the case of a free-shear layer. The degree of organization of the self-excited, resonant-coupled oscillation and the manner in which it varies with open area ratio and geometry of the plate are interpreted in terms of the flow structure on either side of, and within, the slotted plate; these features are compared with the corresponding structure of the free-shear layer oscillations.     

不同剪切率来流作用下柔性圆柱涡激振动数值模拟

采用浸入边界法对细长柔性圆柱在线性剪切流条件下的涡激振动进行三维数值模拟。细长柔性圆柱振动采用三维索模型模拟,其两端铰接,质量比为6,长细比为50,无量纲顶张力为496。来流为线性剪切流,剪切率从0到0.024变化,最大雷诺数为250。研究发现:剪切流作用下柔性立管横流向振动表现为驻波模式,而顺流向振动表现为行波-驻波混合模式。随着剪切率增大,振动频谱呈现多频响应,振动能量逐渐向低频转移。阻力系数平均值随着展向变化,脉动阻力系数和升力系数的均方根值均表现为“双峰”模式。流固能量传递系数沿立管轴向的分布表明,振动激励区集中于高流速区,而振动阻尼区多位于低流速区。剪切率较小时,圆柱的泻涡为平行交叉模式;剪切率较大时,圆柱的泻涡为倾斜泻涡模式,且由于泻涡频率沿立管轴向变化,尾流发生涡裂现象,形成泻涡频率不同的胞格结构。      

Self-sustained oscillations of shear flow past a slotted plate coupled with cavity resonance

Shear flow past a slotted plate configuration can give rise to highly coherent, self-sustained oscillations when coupling occurs with a resonant mode of an adjacent cavity. The distinctive feature of these oscillations is that the wavelength of the coherent instability along the plate is of the order of the plate length. This observation is in contrast to previous investigations of flow past perforated or slotted surfaces, where the instability scales on the diameter of the perforation or the gap length of a slot. The present oscillations occur even when the inflow boundary layer is turbulent and an inflectional form of the shear flow cannot develop along the cavity opening, due to the presence of the slotted plate. Instigation of a resonant mode of the cavity, in conjunction with an inherent instability of the shear flow along the plate, gives rise to ordered clusters of instantaneous vorticity and instantaneous velocity correlation. During the oscillation, ejection of flow occurs from the cavity to the region of the shear flow; this ejection is in accord with the convection of the large-scale cluster of vorticity along the slotted plate. This oscillation can be effectively detuned by adjusting the inflow velocity, such that the inherent instability of the shear flow past the slotted plate is no longer coincident with the resonant frequency of the cavity. Certain features of this self-sustained oscillation are directly analogous to recent findings of oscillations due to shear flow past a perforated plate bounded by a cavity, but in the absence of cavity resonance effects.     

一种基于超声共振谱的低Q值材料共振频率提取方法

超声共振谱技术通过测量样本在超声激励下产生的固有共振频率来计算弹性参数,而共振频率的提取是整个测量过程的关键.低$Q$值(品质因数)材料由于其衰减特性,导致共振谱平缓并无法直观地从谱图上观察得到共振频率,为从中提取更为有效的共振频率, 本文提出了一种新的共振频率提取方法.采用经验模态分解法将材料频率响应自适应分解为有限个具有特殊振荡特性的固有模态函数分量,根据材料的超声共振谱先验信息选择具有共振频率特性的固有模态函数分量,并从中提取共振频率. 以短切纤维环氧树脂材料(仿骨材料, $Q \approx$25)为例, 通过实验与传统线性预测方法进行对比,计算弹性系数和工程模量. 实验结果表明新方法的计算效率高,对弱激发模态更为敏感,共振频率的匹配数量(26)多于传统方法(21)且满足5倍于弹性系数的估计要求,优化后的弹性模量更接近标准值.新方法可从低$Q$值材料平缓的频谱中提取数量足够且有效的共振频率,不仅有效提升了力学参数估计的可靠性,而且拓展了超声共振谱技术的应用范围.      

Exploratory study of turbulent structure of a compressible shear layer using fluctuating pitot pressure measurements

An experimental study has been conducted to determine if two-point fluctuating pitot pressure measurements can be used to detect and quantify the large-scale structures in a two-dimensional, high Reynolds number, supersonic, turbulent shear layer. There is evidence from the two-point correlations of fluctuating pitot pressures and from the VITA analysis that large-scale structures exist and span the thickness of the shear layer. Because the shear layer exhibits a wake-like character, the large-scale structure in the lower part of the shear layer is essentially normal to the flow direction. Power spectra measured at about 25 initial shear layer thicknesses downstream of the origin are broadband, which suggests that the large-scale structures are not yet highly organized.A version of this paper was presented at the 12^th Symposium on Turbulence at the University of Missouri-Rolla     

Instability of the separated shear layer in flow past a cylinder: Forced excitation

The receptivity of the separated shear layer for Re = 300 flow past a cylinder is investigated by forced excitation via an unsteady inflow. In order to isolate the shear layer instability, a numerical experiment is set up that suppresses the primary wake instability. Computations are carried out for one half of the cylinder, in two dimensions. The flow past half a cylinder with steady inflow is found to be stable for Re = 300. However, an inlet flow with pulsatile perturbations, of amplitude 1% of the mean, results in the excitation of the shear layer mode. The frequency of the perturbation of the inlet flow determines the frequency associated with the shear layer vortices. For a certain range of forced frequencies the recirculation region undergoes a low‐frequency longitudinal contraction and expansion. An attempt is made to relate this instability to a global mode of the wake determined from a linear stability analysis. Interestingly, this phenomenon disappears when the outflow boundary of the computational domain is shifted sufficiently downstream. This study demonstrates the need of carefully investigating the effect of the location of outflow boundaries if the computational results indicate the presence of low‐frequency fluctuations. The effect of Re and amplitude of unsteadiness at the inlet are also presented. All computations have been carried out using a stabilized finite element formulation of the incompressible flow equations. Copyright © 2007 John Wiley & Sons, Ltd.