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1.
平稳随机振动荷载识别的逆虚拟激励法(二)   总被引:6,自引:0,他引:6  
本文将逆虚拟激励法(IPEM)用于求解平稳随机振动的荷载谱识别问题,已知部分结构应变(或部分应变及部分位移)响应的自谱与互谱,反求多点激励间的自谱与互谱。  相似文献   

2.
对多支承激励间存在相位差的平稳随机响应分析问题给出了计算各种自谱密度及互谱密度的快速直接算法。此法计入了所有参振振型间的互相关项,以及各激励间的互相关项,是快速、简便、精确的频域分析方法,并可用实振型方便地处理非正交阻尼矩阵。  相似文献   

3.
多相位激励随机地震响应快速算法   总被引:2,自引:0,他引:2  
对多支承激励间存在相位差的平稳随机响应分析问题给出了计算各种自谱密度及互谱密度的快速直接算法。此法计入了所有参振振型间的互相关项,以及各激盛间的互相关项,是快速,简便,精确的频域分析方法,并可用实振型方便地处理非正交阻尼矩阵。  相似文献   

4.
研究了复杂结构的空间部分相干多点激励平稳随机地震响应。该方法同时计入了振型间和激励间的耦合项,是完全的CQC算法,可以方便高效且高精度地算出各种响应量的自谱和互谱。  相似文献   

5.
大跨度结构受多点随机地震激励的响应   总被引:23,自引:0,他引:23  
研究了复杂结构的空间部分相干多点激励平稳随机地震响应,该方法同时计入了振型间和激励间的耦合项,是完全的CQC算法,可以方便高效且高精度地算出各种响应量的自谱和互谱。  相似文献   

6.
关于虚拟激励法与结构随机响应的注记   总被引:48,自引:6,他引:42  
虚拟激励法自发表以来,引起了学术界和工程界的较大关注。特别是在处理大型复杂结构受多点随机激励时,该法自动计及了参振振型的互相关以及激励之间的互相关,在理论上是精确解。而且该法对于处理非经典阻尼矩阵很方便,在一般具有简谐振动/时程分析功能的有限元程序上进一步开发计算位移,内力,应变等各种平稳/非平稳响应量的自谱互谱计算功能都十分方便,所以获得了较多应用。对该算法的适应性和计算效率与传统算法明确地给出对比,将对其理解与推广应用有很大好处。本文将对此作一些说明。  相似文献   

7.
本文提出了基于高频动态测力天平试验的风振响应的频域分析方法,采用该方法可以用来求解复杂高耸结构的三维耦联风振响应,并给出了利用高频动态测力天平试验来确定广义模态力谱的计算方法.该方法利用高频动态测力天平试验得到的基底剪力自谱、基底弯矩自谱以及基底剪力与弯矩的互谱与脉动风荷载的自谱密度的相互关系并通过引入振型修正系数来求得广义模态力谱,求解结构的三维耦联风振响应.然后,采用本文方法对在建的河南省广播电视发射塔的风振响应进行了研究,结果表明横风向的位移和加速度响应的均方根值要大于顺风向,因此在计算中必须考虑横风向风振的影响.最后本文对计算振型数目和模态耦联项对结构风振响应的影响进行了分析.本文的方法对于求解复杂高耸结构的风振响应具有重要的借鉴意义.  相似文献   

8.
多点非均匀调制演变随机激励下结构地震的响应   总被引:1,自引:0,他引:1  
针对大跨度结构在非均匀调制演变随机激励作用下,考虑行波效应时的非平衡随机地震响应问题,应用虚拟激励法进行了分析,由于虚拟激励法自动计及了参振振型的互相关项以及激励之间的互相关项,理论上是精确解,时变功率谱的计算采用精细逐步积分格式,使计算效率进一步得到提高。  相似文献   

9.
线性随机结构在随机激励下动力响应分析   总被引:20,自引:4,他引:16  
李杰  廖松涛 《力学学报》2002,34(3):416-424
利用虚拟激励法对随机结构正交展开理论进行扩展,并在Ritz向量子空间中对扩阶系统方程进行动力聚缩,提出了一类可以快速高效地进行线性随机结构复合随机振动分析的计算方法.算例分析表明,该法可以方便地分析随机结构在平稳或非平稳随机激励下的复合随机振动问题,且分析结果与 Monte Carlo模拟分析结果符合良好;与均值参数确定性结构传统随机振动分析计算结果相比,随机结构在相同随机激励下响应自谱密度曲线具有峰值降低、谱宽增大的特点.  相似文献   

10.
本文首先对平稳随机过程的多输入单输出线性系统建立剩余随机过程。再用最小二乘预测方法,通过剩余过程的相关函数,找到剩余过程的自谱及互谱。定义了偏凝聚函数,并验证其正确性,然后将结果推广到多输入多输出线性系统,最后简述其应用。  相似文献   

11.
Stochastic Analysis of Self-Induced Vibrations   总被引:1,自引:0,他引:1  
Rüdinger  F.  Krenk  S. 《Meccanica》2002,37(1-2):3-14
Vortex-induced vibrations of a structural element are modelled as a non-linear stochastic single-degree-of-freedom system. The deterministic part of the governing equation represents laminar flow conditions with a stationary non-zero solution corresponding to lock-in. Across-wind turbulence is included as an additive excitation and along-wind turbulence is introduced as a parametric excitation term, both assumed to be white noise processes. An approximate closed-form solution to the corresponding Fokker–Planck equation in terms of the stationary probability density of the energy is obtained. The auto spectral density of the position at a particular energy-level is approximated by the spectral density of a linear system with energy dependent damping. The spectral density is then obtained by integration of the energy conditional spectral density over all energies weighted by the probability density. The approximate theoretical expressions for the probability density of the energy and the auto spectral density of the position compare favourably with results obtained by numerical simulation.  相似文献   

12.
Flow transitions occurring with increase in the Taylor number in an annular gap of radius ratio 0.8, having an imposed axial flow of air of Reynolds number 500 have been studies using the output from a cross-wire probe in a complex digital analysis. Cross and phase spectra, together with auto and cross correlograms, are presented for four Taylor numbers from 10 620 to 12.2 × 106, covering the onset of vortex flow, chaotic flow and turbulent vortex flow. As the Taylor number increases, there is little alteration in the spiral vortex flow in the axial and tangential directions, which oscillates in phase in these two directions. The tangential velocity gradient was seen to become increasingly dominant, with increase in the Taylor number  相似文献   

13.
A fully coupled structural–acoustic model of a cylindrical shell under external turbulent boundary layer excitation is herein developed. The numerical process requires computation of the wall pressure cross spectral density function as well as sensitivity functions for the fluid-loaded cylindrical shell. A semi-empirical model from literature is used to describe the wall pressure field induced by the turbulent boundary layer in the wavenumber–frequency domain. An analytical expression of the wall pressure field for a flat surface is adapted to describe the wall pressure field for a cylindrical surface. Circumferential sensitivity functions are derived using a wavenumber-point reciprocity principle. Results for the near-field and far-field acoustic pressure spectra are presented. Contributions of individual circumferential modes to the acoustic pressure spectra are examined, showing distinct trends below and above the ring frequency. The proposed method is computationally efficient and provides an effective approach to investigate vibroacoustic responses for maritime platforms.  相似文献   

14.
桥梁结构移动平稳随机荷载识别新方法   总被引:4,自引:2,他引:2       下载免费PDF全文
移动的平稳随机荷载对简支梁的作用,相当于固定的调制函数已知的非平稳随机荷载对简支梁结构的作用.本文以此为基础,研究了移动平稳随机荷载的识别问题.首先基于虚拟激励法的思想,利用特征值分解及奇异值分解技术,由虚拟位移响应反演虚拟广义坐标,有效地避免了矩阵求逆,得到高精度的广义坐标谱;同时利用Wiener-Khintchine关系及Duhamel积分,由广义坐标谱值反演得到平稳随机激励谱密度.仿真算例表明,只要适当地选取参振振型及测点位置,本文方法可以有效地识别桥梁结构的移动平稳随机荷载.  相似文献   

15.
对包含不同类型裂纹(横裂纹、横-斜裂纹以及任意斜裂纹)的转子的耦合振动进行研究,以揭示裂纹转子在不同方向上刚度参数的变化规律及其交叉耦合机理,特别是由此引发的振动特征. 对于包含不同类型裂纹的转子轴段,采用六自由度Timoshenko梁单元模型对其进行单元建模,并基于应变能理论推导计算柔度参数和刚度矩阵. 在此基础上, 采用纽马克-$\beta$数值算法求解裂纹转子的运动方程,获得裂纹转子在单故障或多故障激励(不平衡激励、扭转激励或不平衡激励加扭转激励)作用下的耦合振动响应,进而分析耦合振动谱特征. 与横裂纹和横-斜裂纹相比,任意斜裂纹使转子刚度矩阵的交叉耦合效应更显著,导致转子发生更强烈的弯-扭耦合甚至是纵-弯-扭耦合振动.无论是在不平衡激励还是扭转激励作用下, 弯曲振动与扭转振动幅度都更大. 而且,包含不同类型裂纹的转子的耦合振动特征频率,例如旋转基频与二倍频、扭转激励频率及其边带成分的幅值,对裂纹面方向角具有不同的敏感性. 所得的这些研究结果,可以为转子裂纹的特征参数辨识与诊断提供理论依据.   相似文献   

16.
参数振动系统响应的频谱成分及其分布规律   总被引:2,自引:0,他引:2  
采用Sylvester理论和Fourier级数展开方法分别研究了参数振动系统自由响应和强迫响应的频谱特性(频谱成分及其分布规律),讨论了系统稳定性和阻尼对于频谱幅值的影响,并给出了系统外激励共振条件.理论研究结果表明:由于参数激励作用使得系统响应具有多频特点,这些频谱成分与系统固有频率、参数激励频率和外激励频率具有密切联系,而且其在频域分布也呈现出一定的规律.此外,参数振动系统具有多个外激励共振点,除了外激励频率等于系统固有频率将发生共振外,当外激励频率等于系统固有频率和参数激励频率的组合值时,同样将发生外激励共振现象.  相似文献   

17.
18.
For fluid-velocity measurements of the two-phase flow in reactor safety experiments, a new method has been developed. This method is based on cross-correlating the signals of two light-beam detectors, which cross the diameter of the test-section (no flow restriction).

Furthermore, the signals of the two detectors are also used to give a rough estimate of the flow-pattern of the investigated two-phase flow. This flow-pattern identification is performed by comparing several characteristic functions (like the spectra and probability-functions of the signals) of a known flow-pattern recorded in an air-water test-facility, with equivalent functions of the investigated two-phase flow. This flow-pattern identification is performed by comparing several characteristic functions (like the spectra and probability-functions of the signals) of a known flow-pattern recorded in an air-water test-facility, with equivalent functions of the investigated two-phase flow. An important requirement for these comparisons is the appropriate normalization of the abscissa of the characteristic-functions, which is performed with the time-averaged fluid velocity.

As an example, the results of a blow-down experiment are shown. Velocities up to 300 m/s could be measured within a pressure range up to 50 bars and temperatures up to 280°C. Flow-regime changes were observed in three different parts of the blow-down.  相似文献   


19.
Roberts  J. B.  Vasta  M. 《Meccanica》2002,37(1-2):33-49
A new energy-based system identification method is developed, applicable in situations where the dynamic response of a structure is measurable but the excitation is unmeasurable and describable only in terms of a stochastic process. It is shown that, in the case of a non-linear single degree of freedom system subjected to purely parametric, non-white random excitation, the power spectrum of the excitation can be identified through an estimation of the diffusion coefficient relating to the energy envelope of the response process. Through an estimation of the drift coefficient an identification of the system damping is also possible. The method is validated through application to simulated data relating to a Duffing oscillator with non-linear damping.  相似文献   

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