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1.
不平衡线性转子-轴承系统的非平稳地震激励响应分析   总被引:2,自引:0,他引:2  
给出了受随机地震激励的线性转子-轴承系统动力响应的有效分析方法。应用虚拟激励法和数值积分法,采用Kanai-Tajimi地震模型,对一个四自由度非对称的刚性转子-轴承系统在地震激励和谐波激励联合作用下的位移响应、位移响应谱密度及响应时变方差进行了分析。讨论了不同转速对位移响应时变方差的影响和不同采样角频率对位移响应时变方差曲线的影响。  相似文献   

2.
多点激励反应谱法的理论研究   总被引:4,自引:0,他引:4  
基于虚拟激励原理建立了多点激励反应谱法。该方法所表示的结构地震动反应由三部分组成,即拟静力响应、动力响应及二者的耦合响应,其中拟静力响应是由地面各点输入位移不一致引起的;动力响应主要是由结构在地面加速度作用下引起的;当结构自振周期小于2s时,拟静力响应与动力响应之间的耦合项可以忽略。该方法计算公式形式简洁,物理意义明确,且与我国现行《抗震规范》中的一致激励反应谱建立了定量关系。在推导过程中,未做任何特殊简化,因而该方法在理论上是严密的。  相似文献   

3.
本文用虚拟激励法结合等效线性法来求解受多相位平稳随机激励的多自由度Duffing系统,过程简洁,计算高效,给出了在该激励下多自由度Duffing系统的数值模拟算法,二者进行了比较,得到了比较满意的结果。  相似文献   

4.
随机激励的耗散的哈密尔顿系统的平稳解   总被引:2,自引:0,他引:2  
朱位秋 《力学学报》1993,25(6):676-684
本文首先为一般的随机激励的耗散的哈密尔顿系统得到精确的平稳解,然后在此基础上为类似而更为一般的系统发展了等效非线性系统法  相似文献   

5.
任意激励下结构动力响应的状态方程精细积分法   总被引:6,自引:1,他引:6  
王忠  王雅琳等 《计算力学学报》2002,19(4):419-422449
对只有弹性模态以及除此之外还有刚体模态的结构的瞬态响应给出了精细积分的通用公式,从而使得该方法不仅可以处理线性激励的情形,而且对激励是多项式形式或可以展开成多项式的激励也同样能够计算。对于非线性激励,只要可以用关于自变量的级数形式来近似表示,都可以用本文所给的方法进行计算,计算的精度可以通过变化级数的项数来调整。  相似文献   

6.
硬弹簧Duffing方程的全局分叉   总被引:4,自引:0,他引:4  
本文采用Melnikov方法讨论硬弹簧系统在周期外激励与参数激励作用下的全局分叉,给出了相应的结论。  相似文献   

7.
参-强激励联合作用下输流管的分岔和混沌行为研究   总被引:4,自引:0,他引:4  
研究输送脉动流的两端固定输流管道在其基础简谐运动激励下的分岔和混沌行为,考虑管道变形的几何非线性和管道材料的非线性因素,推导了系统的非线性运动方程,并应用Galerkin方法对其进行了离散化处理。通过采用数值模拟方法,对系统的运动响应进行仿真,重点探讨了流体平均流速、流速脉动振幅以及基础简谐运动激励振幅对系统动态特性的影响。结果表明,系统在不同的参数下会发生围绕不同平衡点的周期和混沌等运动,并在系统中发现了两条通向混沌运动的途径:倍周期分岔和阵发混沌运动。  相似文献   

8.
基于复模态分析和虚拟激励法.提出了用于具有密集频率和非经典阻尼受控结构风振响应分析的广义虚拟激励法。该法可以考虑任意风谱和空间相关性以及模态耦合效应,且计算效率很高。不同于SRSS法.该算法包含了全部参振模态之间和全部激励点之间的相关性.在理论上是精确解。  相似文献   

9.
可调磁流变阻尼在汽车悬架的半主动控制中的应用   总被引:2,自引:0,他引:2  
本文研究了采秀磁流变阻尼的汽车半主动控制悬架在确定性激励和随机激励下的运行效果,分析了可调磁流变阻尼半主动控制的控制规律及响应情况,并与采用传统阻尼的汽车被动悬架和主动悬架进行了对比,证实了磁流变阻尼应用于汽车半主动控制的可行性及优越性。  相似文献   

10.
行波效应下结构非平稳随机地震峰值响应分析   总被引:3,自引:0,他引:3  
地震运动在本质上是非平稳随机过程。对于一个典型的地震记录,如果地震平稳段持续时间较短,采用非平稳随机过程描述其地震动特性较为合理。目前被最广泛接受的地震非平稳随机振动模型是演变随机激励模型。本文将虚拟激励法和精细积分法相结合,高精度计算了结构在这种随机地震激励下的时变均方根响应,并等效转化为相应的平稳随机过程后进行结构峰值响应计算。不仅考虑了激励的非平稳性,同时高效精确地考虑了结构的动力特性和地震行波效应。能够方便地应用于大型复杂结构,特别是为大跨度桥梁抗震分析提供了高效的计算手段。实际结构算例表明平稳假设会得到偏于保守的结果。当阻尼比较小时,这种差别会更明显。采用非平稳激励模型,显然更为合理;采用本文提出的方法可以很方便地处理这类问题。  相似文献   

11.
ROSSBY WAVES WITH THE CHANGE OF β   总被引:3,自引:0,他引:3  
In this paper, the change of the Rossby parameter β with latitude is considered and the parameter γ≡-dβ/dy=2sinφ/a2 is introduced and the β-plane approximation is extended into f=f00y-γ0y2/2 which includes the parameter γ. Such approximation closes further to practice especially in the high latitude regions.We give emphasis to the research of the effect of the parameter γ on the Rossby waves. It is seen that the effect of the parameter γ is remarkable in the high latitude regions. It can produce the Rossby waves caused by the pure parameter γ. And the phase speed formula of Rossby waves with the change of ft is generally given, which is degenerated into the well-known Rossby formula when γ0=0. The researches also point out that when the change of β is regarded, even if the basic current u is a linear function of y the unstable modes can also take place. However,the parameter γ usually plays a stable part in the Rossby waves and it does affect the longitudinal scale and the structure of constant phase lines(trough-ridge lines)of Rossby waves and slow down the growing or decaying of Rossby waves.  相似文献   

12.
The onset of double diffusive convection in a two component couple stress fluid layer with Soret and Dufour effects has been studied using both linear and non-linear stability analysis. The linear theory depends on normal mode technique and non-linear analysis depends on a minimal representation of double Fourier series. The effect of couple stress parameter, the Soret and Dufour parameters, and the Prandtl number on the stationary and oscillatory convection are presented graphically. The Dufour parameter enhances the stability of the couple stress fluid system in case of both stationary and oscillatory mode. The effect of positive Soret parameter is to destabilize the system in case of stationary mode while it stabilizes the system in case of oscillatory mode. The negative Soret parameter enhances the stability in both stationary and oscillatory mode. The couple stress parameter enhances the stability of the system in both stationary and oscillatory modes. The Dufour parameter increases the heat transfer while the couple stress parameter has reverse effect. The Soret parameter has negligible influence on heat transfer. Both Dufour and Soret parameters increases the mass transfer while the couple stress parameter has dual effect depending on the value of the Rayleigh number.  相似文献   

13.
Effect of ion‐slip current on the thermal instability in a boundary layer is studied. The criterion on the position marking the onset of longitudinal vortices is defined in the present paper. The results show that the onset position characterized by the Grashof number depends on the Prandtl number, the Reynolds number, the wave number, the Hall parameter, the ion‐slip parameter, and the Hartmann number. The flow becomes more stable as the magnetic field increases. However, the destabilizing effects are found on the flow when the Hall and ion‐slip currents are presented. The results of the present numerical prediction show reasonable agreement with the experimental data in the case of zero Hartmann number, ion‐slip parameter, and Hall parameter in the open literature. Copyright © 2011 John Wiley & Sons, Ltd.  相似文献   

14.
本文发展了一类新的动力系统参数识别方法。通过引入微分算子变换,使系统状态变量与系统参数成功地分离开来。然后,以算子变换方程作为观测方程,并引入关于系统参数的状态方程;利用广义卡尔曼滤波方法进行参数递推估计。系统仿真算例表明:本文建议的新方法,不仅可以适用于较高噪声环境情形,而且可以同时适用于线性参数系统与非线性参数系统。  相似文献   

15.
在销-盘式摩擦磨损试验机上对船用柴油机活塞环-缸套材摩擦副进行磨合磨损试验,采用光学显微镜对不同磨损阶段的磨损表面形貌进行观察分析,应用小波分析和奇异值分解提取磨损表面统计特征的低频特征参数和高频特征参数.结果表明:低频特征参数和高频特征参数刻画了磨合表面的形貌特征,可以作为磨合表面的特征参数;低频特征参数反映了磨合表面的接触面积,其值愈大,接触面积愈大;高频特征参数反映了磨合表面的粗糙度,其值愈大,粗糙度愈小.  相似文献   

16.
An analysis of steady laminar mixed-convection heat transfer from a rotating or nonrotating axisymmetric body is presented. A mixed-convection parameter is proposed to serve as a controlling parameter that determines the relative importance of the forced and the free convection. In addition, a rotation parameter is introduced to indicate the relative contributions of the flow forced convection and the rotational forced convection. The values of both these two parameters lie between 0 and 1. Furthermore, the coordinates and dependent variables are transformed to yield computationally efficient numerical solutions that are valid over the entire range of mixed convection from the forced-convection limit (rotating or nonrotating bodies) to the pure free-convection limit (non-rotating bodies) and the entire regime of forced convection from the pure flow forced-convection limit (nonrotating bodies) to pure rotational forced-convection limit (rotating bodies). The effects of mixed-convection intensity, body rotation, fluid suction or injection, and fluid Prandtl number on the velocity profiles, the temperature profiles, the skin-friction parameter, and heat transfer parameter are clearly illustrated for both cases of buoyancy assisting and opposing flow conditions.  相似文献   

17.
The parametric excited vibration of a pipe under thermal loading may occur because the fluid is often transported heatedly. The effects of thermal loading on the pipe stability and local bifurcations have rarely been studied. The stability and the local bifurcations of the lateral parametric resonance of the pipe induced by the pulsating fluid velocity and the thermal loading are studied. A mathematical model for a simply supported pipe is developed according to the Hamilton principle. Two partial differential equations describing the lateral and longitudinal vibration are obtained. The singularity theory is utilized to analyze the stability and the bifurcation of the system solutions. The transition sets and the bifurcation diagrams are obtained both in the unfolding parameter space and the physical parameter space, which can reveal the relationship between the thermal field parameter and the dynamic behaviors of the pipe. The frequency response and the relationship between the critical thermal rate and the pulsating fluid velocity are obtained. The numerical results demonstrate the accuracy of the single-mode expansion of the solution and the stability and local bifurcation analyses. It also confirms the existence of the chaos. The presented work can provide valuable information for the design of the pipeline and the controllers to prevent the structural instability.  相似文献   

18.
航空发动机涡轮盘裂纹萌生寿命的估算方法   总被引:1,自引:0,他引:1  
针对航空发动机涡轮盘裂纹萌生寿命的估算问题,给出一个全新的损伤参量。该损伤参量结合了分析多轴疲劳的临界面方法,“应力功”的概念和疲劳破坏的微观机制。依据该损伤参量,利用有限元程序和自编程序计算得出损伤参量和疲劳循环次数的关系,建立以这一损伤参量为基础的疲劳损伤累积模型,进而估算涡轮盘裂纹萌生寿命。  相似文献   

19.
谱载荷下疲劳裂纹扩展随机规律的实验研究   总被引:2,自引:0,他引:2  
简要介绍了谱载荷下疲劳裂纹扩展试验的理论基础、方法和过程。讨论了各种数据处理方法对参数估计的影响,研究了疲劳裂纹扩展的随机规律。由试验得到的疲劳裂纹扩展试验数据估计了裂纹扩展方程的参数,计算出结构可靠度曲线,通过对试验结果的分析难证了以下结论:以时间为参量的裂纹扩展随机过程模型和以裂纹长度为参量的模型在一定条件下是统一的;数据处理方法的选择与可靠性分析的结果有密切的联系;裂纹扩展寿命受裂纹扩展队机  相似文献   

20.
This paper shows that a numerical modelling method in which constraints are replaced with positive and negative penalty functions, which may be regarded as artificial elastic restraints of positive and negative stiffness, may be safely used to determine the critical speed associated with aeroelastic divergence. The critical speeds of a beam with restraints of positive and negative stiffness are found to converge to that of the constrained system, from below if the stiffness is positive and from above otherwise. A uniform Euler–Bernoulli beam clamped at the rear end is analysed using an artificial restraint to enforce the constraint of zero rotation at the clamp, and the results are compared with the exact critical speed of the constrained system obtained analytically. The paper shows that, contrary to common belief that the penalty parameter must be positive, the inclusion of a negative penalty parameter enables the determination of errors due to violation of the constraints.  相似文献   

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