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 共查询到19条相似文献,搜索用时 78 毫秒
1.
变质量,变阻尼,变刚度结构系统的动力响应   总被引:4,自引:0,他引:4  
本文首次提出了变质量、变阻尼、变刚度结构系统的动力响应问题,并根据抓斗卸船机的工作过程导出了结构系统的动力方程及解法。最后给出了工程实际算例。  相似文献   

2.
本文用矩量法解薄板塑性动力响应问题,分析阻尼介质对简支方板塑性动力响应的影响,对计算结果进行了讨论.  相似文献   

3.
本文导出具有非比例阻尼的线性系统在一般激励下解的形式,给出了一种近似解法,並以简谐激励为例进行讨论。  相似文献   

4.
本文用矩量法解薄板塑性动力响应问题,分析阻尼介质对简支方板塑性动力响应的影响,对计算结果进行了讨论。  相似文献   

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通过Laplace 变换,用矩量法求解弹性基础上简支方板在阻尼介质中的塑性动力响应,得出解析表达式。  相似文献   

8.
冲击载荷作用下阻尼介质中刚塑性圆板的动力响应   总被引:4,自引:1,他引:4  
1.引言阻尼介质对结构塑性动力响应的影响属于流体与固体的耦合运动。在分析中往往将流体对固体的作用采用一个相当的阻力来代替。当流体为水时,这一阻力可表示为f=α(?)。其中,f为圆板单位面积上流体阻力;α为阻尼系数,它与流体介质密度及其波速有关;(?)为圆板横向速度。Kumar在1982年曾采用此方法得到了矩形载荷作用下简支圆板在阻尼介质中的动力响应完全解。但同样的结果早在1963年就由苏联学者  相似文献   

9.
本文应用最小二乘法,分析了阻尼介质对简支圆柱壳塑性动力响应的影响。  相似文献   

10.
爆炸荷载作用下弹性与阻尼支承梁的动力响应   总被引:17,自引:0,他引:17  
为了提高梁的抗爆能力,目前通常是从材料、截面形状等方面考虑.通过在梁端部设置弹性和阻尼支承来提高梁的抗力.为此,应用拉格朗日方程建立了端部弹性与阻尼支承梁的动力方程,通过长作用时间和短作用时间两个爆炸动荷载的典型算例,分析了端部弹性与阻尼支承对梁动态响应的影响,并指出在短作用时间动荷载作用下在梁端部设置弹性与阻尼支承可有效提高梁的抗力.  相似文献   

11.
In this paper, a new method, the step-reduction method, is proposed to investigate the dynamic response of the Bernoulli-Euler beams with arbitrary nonhomogeneity and arbitrary variable cross-section under arbitrary loads. Both free vibration and forced vibration of such beams are studied. The new method requires to discretize the space domain into a number of elements. Each element can be treated as a homogeneous one with uniform thickness. Therefore, the general analytical solution of homogeneous beams with uniform cross-section can be used in each element. Then, the general analytic solution of the whole beam in terms of initial parameters can be obtained by satisfying the physical and geometric continuity conditions at the adjacent elements. In the case of free vibration, the frequency equation in analytic form can be obtained, and in the case of forced vibration, a final solution in analytical form can also be obtained which is involved in solving a set of simultaneous algebraic equations with only  相似文献   

12.
THEGENERALSOLUTIONFORDYNAMICRESPONSEOFNONHOMOGENEOUSBEAMWITHVARIABLECROSSSECTIONJiZhen-yi(纪振义)(AnhuiArchitecturalIndustryColl...  相似文献   

13.
结构动力响应精细时程法的并行算法分为两类:基于特解的并行算法和基于直接积分法的并行算法;后者因为不需知道荷载的具体形式而更具应用价值。精细时程法的时程积分由齐次方程的通解和非齐次项的积分构成,基于直接积分法的并行算法很好地并行了非齐次项的积分,而对通解项采用串行计算。设计了一种不均衡步数的负载分配策略,能够减少处理器等待自身初值的时间,相对均衡步数的分配策略,能够获得更高的加速比,给出了相应的证明和算例验证。  相似文献   

14.
Summary In this paper, the influence of the variable stiffness of mating gear teeth on dynamic loads occurring between teeth in a single-gear transmission is investigated using a discrete-continuous model consisting of two torsionally deformable ponderable shafts and four rigid bodies. The stiffness is described by a harmonic function of time. Considerations by means of the wave method enable to determine dynamic loads in steady as well as in transient states. Numerical calculations are concentrated on the determination of the amplitudes of dynamic loads on gear teeth with respect to revolution per minute. Received 4 March 1997; accepted for publication 12 September 1997  相似文献   

15.
A theoretical analysis is presented for the dynamic plastic behavior of a simplysupported rigid,perfectly plastic circular plate in damping medium with finite-deflectionssubjected to a rectangular pressure pulse.Analytical solutions of every moving stage underboth medium and high loads are developed.  相似文献   

16.
1.IntroductionMoreandmoreattentionhasbeenpaidtothestudyofdynamicsofcomplicatedsystemwiththedevelopmentofmodernscienceandtechnology.Thestudyoftherelativemotionofvariablemasssystembyusingthetheoryandmethodofanalyticalmechanicsnotonlycanunifytheexpressionformbutalsocandisplayitssuperioritytothecomplicatedsystem.In1961,thedynamicsofrelativemotionofholonomicsystemwasderivedbyLur'ell].Inrecehtyears,LiulZIandLuol3'4]havegiventhedynamicsequationsofrelativemotionofvariablemassnonholonomicsystem.Howe…  相似文献   

17.
This paper presents a mathematical study on the subsonic aerodynamics acting on an airfoil with a cubic stiffness. One portion of aerodynamics is assumed as and replaced by an equivalent damping. Using the harmonic balance method, an equivalent system is deduced and studied by a numerical integration method. Numerical examples show the validity and feasibility of the proposed mathematical treatment of the aerodynamics. It reveals that the unsteady aerodynamics acting on the airfoil can not only affect the pitch stiffness but also result in additional damping.  相似文献   

18.
利用Laplace—Hankel联合积分变换,推导出了单层粘弹性半空间轴对称问题在动荷载作用下,层间完全接触情况的刚度矩阵,然后按传统的有限元方法组成总体刚度矩阵。通过求解由总体刚度矩阵所构成的代数方程就可解出动荷载作用下多层粘弹性半空间轴对称问题的矩阵。由于刚度矩阵的元素中只含有负指数项,计算时不会出现溢出的现象。本文还成功地应用了Durbin的Laplace逆变换的数值方法,求解出了多层粘弹性体的时域解。最后,文中还给出了路面动弯沉的计算结果与实测结果的对比来证明推导结果的准确性。  相似文献   

19.
变截面构件在工程中应用广泛,在对变截面梁进行数值计算时,需要建立变截面梁单元的刚度矩阵。该文采用势能驻值原理,考虑了轴力引起的几何非线性和剪切变形的影响,将梁截面刚度的变化率作为小量,得到了近似到二阶的单元刚度矩阵。在构造位移模式时,从梁的微分平衡方程出发,得到同样近似到二阶、分别以三次和五次多项式表示的剪切和弯曲位移模式。该文还证明了单元刚度矩阵的奇异性,给出了轴压刚度的表达式,定量论证了与某些精确解的误差,表明在一定范围内,该文的结果具有足够的精度。最后以一个计算实例说明该文的单元刚度矩阵具有较快的收敛性。  相似文献   

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