WO2021082959A1 - Nonlinear dynamic time history analysis method for complex building structure - Google Patents

Nonlinear dynamic time history analysis method for complex building structure Download PDF

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WO2021082959A1
WO2021082959A1 PCT/CN2020/121713 CN2020121713W WO2021082959A1 WO 2021082959 A1 WO2021082959 A1 WO 2021082959A1 CN 2020121713 W CN2020121713 W CN 2020121713W WO 2021082959 A1 WO2021082959 A1 WO 2021082959A1
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analysis method
building structure
history analysis
nonlinear
complex building
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徐俊杰
黄羽立
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李鲁
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    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/13Architectural design, e.g. computer-aided architectural design [CAAD] related to design of buildings, bridges, landscapes, production plants or roads
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]

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  • the invention belongs to the technical field of building structure design, and specifically relates to a fast analysis method for nonlinear dynamic time history analysis of complex building structures under dynamic external loads.
  • the domestic building structure design code requires that, in the design stage, a nonlinear dynamic time history analysis of complex building structures is required to better grasp the seismic capacity of the structure, and thereby ensure the safety of the structure under the action of an earthquake.
  • Structural nonlinear dynamic time history analysis is a spatial discrete model of building structure.
  • the differential equations of the motion of each particle are solved to obtain the displacement, velocity, and acceleration response of each particle in the model, and then the model is obtained.
  • the peak values of axial force, shear force and bending moment of each component are used to guide the design of the component section.
  • the existing technology mainly uses two types of methods for dynamic time history analysis of complex building structures.
  • One type is an explicit method, such as the central difference method.
  • the explicit method is stable and the time step of the analysis is limited by the highest frequency of the model.
  • the highest frequency is very large, and when the model has zero mass degrees of freedom or rigid connections, the frequency is infinite, and the explicit algorithm fails.
  • the other type of methods are implicit methods, such as Newmark method, HHT method, generalized ⁇ method, etc. These methods are all unconditionally stable methods, which are suitable for dynamic analysis of complex structures. However, when these methods are used for nonlinear dynamic time history analysis When, non-linear iteration cannot be avoided.
  • the purpose of the present invention is to make two key improvements to the nonlinear iterative process of the Newmark method and provide a A fast analysis method for nonlinear dynamic time history analysis of complex building structures under dynamic external loads.
  • a method for nonlinear dynamic time history analysis of complex building structures is a fixed iteration number analysis method for nonlinear dynamic time history analysis of complex building structures under earthquake action. The steps are as follows:
  • the first step is to perform spatial finite element discretization of the complex building structure, and establish a finite element model discrete system for the building structure.
  • the beams and columns adopt fiber beam models, and the shear walls and floor slabs adopt layered shell elements and Rayleigh damping.
  • the element damping matrix integrates the overall stiffness matrix, the overall mass matrix and the overall damping matrix by the element stiffness matrix, the element mass matrix and the element damping matrix, and the motion equations of the discrete system are derived from the Hamilton principle, and the motion equations of the discrete system are established:
  • u, And ü are the displacement, velocity and acceleration vectors of each particle of the finite element model
  • M is the mass matrix
  • C is the damping matrix
  • F S is the nonlinear restoring force, which is the nonlinear function of the displacement vector
  • the second step is to select parameters and determine global invariants:
  • K 0 is the Jacobian matrix of the nonlinear restoring force F S (u) at u 0 , that is, the initial stiffness matrix;
  • Step-by-step calculation time the end of each time step is calculated time displacements, velocity and acceleration for the i-th time step, known at time i t displacement velocity V i and u i, is calculated by the i Displacement u i+1 and velocity at t i+1 on two time steps And acceleration ü i+1 ;
  • the value range of ⁇ is ⁇ 0.5.
  • is taken as 0.5.
  • the value range of ⁇ is ⁇ 0.25.
  • is taken as 0.25.
  • the value range of ⁇ is ⁇ 1.
  • is taken as 1.
  • the time step ⁇ t is taken as N times the time interval of the base input acceleration record ü g , and N is a positive integer, preferably 1.
  • n takes 2 in the n non-linear iterations.
  • the present invention has the advantages of:
  • the fast dynamic time history analysis method of the present invention only uses the initial stiffness matrix K 0 and does not need the tangent stiffness matrix K T. Therefore, it is not necessary to update the equivalent stiffness matrix. It is only necessary to calculate the equivalent stiffness matrix before the time step calculation. Triangular decomposition can be performed once, which avoids the traditional method of recalculating and decomposing a large number of calculations of the equivalent stiffness matrix at each time step.
  • the present invention adopts the initial stiffness matrix amplification factor ⁇ .
  • the value of ⁇ 1 can be selected to ensure the unconditional stability of the algorithm.
  • the fast dynamic time history analysis method of the present invention only needs to perform a fixed number of nonlinear iterations at each time step, generally two times, which avoids the huge amount of calculation consumed by the traditional method to iterate to meet the tolerance.
  • the fast dynamic time history analysis method of the present invention has a second-order accuracy, which is equivalent to the accuracy of the traditional Newmark method.
  • the dynamic time history analysis method of the present invention has simple steps, only needs to modify the equivalent stiffness update mechanism of the traditional Newmark method, and restricts the number of iterations, even without the need to prepare a new program, and is easy to popularize and apply.
  • FIG. 1 Schematic diagram of complex high-rise structure
  • FIG. 1 Schematic diagram of El-Centro wave
  • FIG. 3 A comparison schematic diagram of the horizontal x-direction displacement of the roof calculated by the Newmark method and the dynamic time history analysis method of the present invention
  • Fig. 4 A comparison schematic diagram of the horizontal x-direction velocity on the roof of a building calculated by the Newmark method and the dynamic time history analysis method of the present invention
  • Fig. 5 A comparison schematic diagram of the vertical x-direction acceleration on the roof of a building calculated by the Newmark method and the dynamic time history analysis method of the present invention
  • the complex high-rise building is shown in Figure 1.
  • the dynamic time history analysis method includes the following steps:
  • the first step is to carry out spatial finite element discretization of the high-rise building to establish a finite element model discrete system of the building structure;
  • the high-rise building includes 23945 nodes, 9744 fiber beam elements defined by 8244 reinforced concrete members and 4704 layered shell elements defined by 177 shear wall components; fiber beam models are used for beams and columns, layered shell elements are used for shear walls and floor slabs, and Rayleigh damping is used to establish element damping matrix, which is composed of element stiffness matrix and element mass matrix
  • the overall stiffness matrix, overall mass matrix and overall damping matrix are integrated with the element damping matrix, and the motion equations of the discrete system are derived from the Hamilton principle, and the motion equations of the discrete system are established:
  • ü are the displacement, velocity and acceleration vectors of each particle of the finite element model.
  • M is the mass matrix
  • C is the damping matrix
  • F S is the nonlinear restoring force, which is the nonlinear function of the displacement vector.
  • ü g uses the El Centro seismic wave shown in Figure 2.
  • the acceleration recording interval is 0.01s
  • the discrete process of this step space finite element method is a widely used routine operation, and the details will not be repeated here.
  • a damping ratio of 5% is used, and the first and ninth modes are selected to calculate the Rayleigh damping coefficient, including mass damping and initial stiffness proportional damping.
  • the second step is to select parameters and determine global invariants:
  • ⁇ 0.5, generally 0.5;
  • is ⁇ 0.25, generally 0.25;
  • is ⁇ 1, and it is generally 1;
  • K 0 is the Jacobian matrix of the nonlinear restoring force F S (u) at u 0 , that is, the initial stiffness matrix.
  • Step-by-step calculation time the end of each time step is calculated time displacements, velocity and acceleration for the i-th time step, known at time i t displacement velocity V i and u i, is calculated by the i Displacement u i+1 and velocity at t i+1 on two time steps And acceleration ü i+1 ;
  • the comparative example adopts the most commonly used second-order precision Newmark method for analysis.
  • the analysis result is shown in Figure 3-5.
  • the calculation time is 300 hours.
  • the dynamic time history analysis method of the present invention the result is very close to the result using the Newmark method (the two response curves almost overlap), and the specific results are shown in Figures 3-5.
  • the calculation time using the method of the present invention is only 5 hours. Under the premise of ensuring the calculation efficiency, the dynamic time history analysis method of the present invention greatly reduces the calculation workload and increases the calculation efficiency by 60 times.
  • the fast dynamic time history analysis method of the present invention only uses the initial stiffness matrix K 0 and does not need the tangent stiffness matrix K T. Therefore, it is not necessary to update the equivalent stiffness matrix. It is only necessary to calculate the equivalent stiffness matrix before the time step calculation. Triangular decomposition can be performed once, which avoids the traditional method of recalculating and decomposing a large number of calculations of the equivalent stiffness matrix at each time step.
  • the present invention adopts the initial stiffness matrix amplification factor ⁇ .
  • the value of ⁇ 1 can be selected to ensure the unconditional stability of the algorithm.
  • the fast dynamic time history analysis method of the present invention only needs to perform a fixed number of nonlinear iterations at each time step, generally two times, which avoids the huge amount of calculation consumed by the traditional method to iterate to meet the tolerance.
  • the fast dynamic time history analysis method of the present invention has a second-order accuracy, which is equivalent to the accuracy of the traditional Newmark method.
  • the dynamic time history analysis method of the present invention has simple steps, only needs to modify the equivalent stiffness update mechanism of the traditional Newmark method, and restricts the number of iterations, even without the need to prepare a new program, and is easy to popularize and apply.

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Abstract

A nonlinear dynamic time history analysis method for a complex building structure. The method comprises the following steps: step one, performing spatial finite element discretization on a complex building structure, and establishing a motion equation set of a discrete system; step two, selecting parameters and determining a global invariant; and step three, performing calculation by time steps, and calculating the displacement, speed and acceleration at an end moment of each time step. In the method, two key improvements are made to the nonlinear iteration process of a Newmark method, such that the calculation workload is greatly reduced and the calculation efficiency is improved on the premise of ensuring the precision of calculations.

Description

一种复杂建筑结构非线性动力时程分析方法A nonlinear dynamic time-history analysis method for complex building structures 技术领域Technical field
本发明属于建筑结构设计技术领域,具体涉及一种用于动力外荷载作用下复杂建筑结构非线性动力时程分析的快速分析方法。The invention belongs to the technical field of building structure design, and specifically relates to a fast analysis method for nonlinear dynamic time history analysis of complex building structures under dynamic external loads.
背景技术Background technique
近年来,地震频发,造成了建筑结构损伤甚至倒塌,严重威胁着国民的生命财产安全。因而,国内建筑结构设计规范要求,在设计阶段,对复杂建筑结构进行非线性动力时程分析,以更好的把握结构的抗震能力,进而确保地震作用下结构的安全。In recent years, earthquakes have occurred frequently, causing structural damage and even collapse of buildings, seriously threatening the safety of people’s lives and property. Therefore, the domestic building structure design code requires that, in the design stage, a nonlinear dynamic time history analysis of complex building structures is required to better grasp the seismic capacity of the structure, and thereby ensure the safety of the structure under the action of an earthquake.
结构非线性动力时程分析,是对建筑结构的空间离散模型,在整个地震作用时间历程上,求解各质点运动的微分方程组,得到模型中各个质点的位移、速度、加速度响应,进而获得模型各个构件的轴力、剪力和弯矩峰值,用于指导构件截面设计。Structural nonlinear dynamic time history analysis is a spatial discrete model of building structure. In the entire seismic time history, the differential equations of the motion of each particle are solved to obtain the displacement, velocity, and acceleration response of each particle in the model, and then the model is obtained The peak values of axial force, shear force and bending moment of each component are used to guide the design of the component section.
目前现有技术针对复杂建筑建筑结构进行动力时程分析主要采用两类方法,一类是显式方法,如中心差分法,然而显式方法条件稳定,分析的时间步长受模型最高频率限制,大规模结构模型,最高频率非常大,且当模型存在零质量自由度或者刚性连接时,频率无穷大,显式算法失效。另一类方法是隐式方法,如Newmark法,HHT法,广义α法等,这些方法均为无条件稳定方法,适用于复杂结构的动力分析,然而,当这些方法用于非线性动力时程分析时,无法避免非线性迭代。因为复杂建筑结构构件数量庞大,其精细化的有限元模型具有海量自由度,加之非线性迭代,造成了分析过程时间耗费巨大,对于一般的复杂建筑结构,一次动力时程分析往往持续十几个小时甚至几天,严重阻碍着复杂建筑结构研究与设计。At present, the existing technology mainly uses two types of methods for dynamic time history analysis of complex building structures. One type is an explicit method, such as the central difference method. However, the explicit method is stable and the time step of the analysis is limited by the highest frequency of the model. For large-scale structural models, the highest frequency is very large, and when the model has zero mass degrees of freedom or rigid connections, the frequency is infinite, and the explicit algorithm fails. The other type of methods are implicit methods, such as Newmark method, HHT method, generalized α method, etc. These methods are all unconditionally stable methods, which are suitable for dynamic analysis of complex structures. However, when these methods are used for nonlinear dynamic time history analysis When, non-linear iteration cannot be avoided. Because of the large number of complex building structure components, its refined finite element model has a large number of degrees of freedom, and nonlinear iterations, resulting in a huge time-consuming analysis process. For general complex building structures, a dynamic time history analysis often lasts more than a dozen Hours or even days, seriously hindering the research and design of complex building structures.
发明内容Summary of the invention
针对现有复杂建筑结构的动力时程分析方法在计算量、求解效率、结果精度方面存在的不足,本发明的目的在于对Newmark法的非线性迭代过程进行两处关键的改进,提供一种用于动力外荷载作用下复杂建筑结构非线性动力时程分析的快速分析方法。In view of the shortcomings of the existing dynamic time history analysis methods of complex building structures in terms of calculation amount, solution efficiency, and result accuracy, the purpose of the present invention is to make two key improvements to the nonlinear iterative process of the Newmark method and provide a A fast analysis method for nonlinear dynamic time history analysis of complex building structures under dynamic external loads.
本发明的技术方案如下:The technical scheme of the present invention is as follows:
一种复杂建筑结构非线性动力时程分析方法,所述方法是一种用于地震作用下复杂建筑结构非线性动力时程分析的固定迭代次数分析方法,其步骤如下:A method for nonlinear dynamic time history analysis of complex building structures. The method is a fixed iteration number analysis method for nonlinear dynamic time history analysis of complex building structures under earthquake action. The steps are as follows:
第一步,对所述复杂建筑结构进行空间有限元离散,建立该建筑结构的有限元模型离散系统,梁柱采用纤维梁模型,剪力墙和楼板采用分层壳单元,并采用Rayleigh阻尼建立单元阻尼矩阵,由单元刚度矩阵、单元质量矩阵和单元阻尼矩阵集成整体刚度矩阵、整体质量矩阵和整体阻尼矩阵,并由Hamilton原理导出离散系统的运动方程组,建立离散系统的运动方程组:The first step is to perform spatial finite element discretization of the complex building structure, and establish a finite element model discrete system for the building structure. The beams and columns adopt fiber beam models, and the shear walls and floor slabs adopt layered shell elements and Rayleigh damping. The element damping matrix integrates the overall stiffness matrix, the overall mass matrix and the overall damping matrix by the element stiffness matrix, the element mass matrix and the element damping matrix, and the motion equations of the discrete system are derived from the Hamilton principle, and the motion equations of the discrete system are established:
Figure PCTCN2020121713-appb-000001
Figure PCTCN2020121713-appb-000001
其中,u,
Figure PCTCN2020121713-appb-000002
和ü分别为有限元模型各质点的位移,速度,加速度向量;M为质量矩阵,C为阻尼矩阵,F S为非线性回复力,是位移向量的非线性函数;P为外部动力荷载,地震作用时,P=-Mü g,ü g为建筑结构基底输入的地震动加速度;
Where u,
Figure PCTCN2020121713-appb-000002
And ü are the displacement, velocity and acceleration vectors of each particle of the finite element model; M is the mass matrix, C is the damping matrix, F S is the nonlinear restoring force, which is the nonlinear function of the displacement vector; P is the external dynamic load, earthquake When applied, P=-Mü g , ü g is the ground motion acceleration input from the base of the building structure;
第二步,选取参数和确定全局不变量:The second step is to select parameters and determine global invariants:
1)选取γ、β、σ;1) Select γ, β, σ;
2)选取时间步长Δt;2) Select the time step Δt;
3)根据已知的初始位移u 0和初始速度
Figure PCTCN2020121713-appb-000003
确定初始加速度ü 0
3) According to the known initial displacement u 0 and initial velocity
Figure PCTCN2020121713-appb-000003
Determine the initial acceleration ü 0 ;
Figure PCTCN2020121713-appb-000004
Figure PCTCN2020121713-appb-000004
4)计算等效刚度矩阵
Figure PCTCN2020121713-appb-000005
4) Calculate the equivalent stiffness matrix
Figure PCTCN2020121713-appb-000005
Figure PCTCN2020121713-appb-000006
Figure PCTCN2020121713-appb-000006
其中,K 0为非线性回复力F S(u)在u 0处雅可比矩阵,即初始刚度矩阵; Among them, K 0 is the Jacobian matrix of the nonlinear restoring force F S (u) at u 0 , that is, the initial stiffness matrix;
第三步,逐时间步计算,计算每个时间步结束时刻的位移、速度和加速度,对于第i个时间步,已知t i时刻的位移u i和速度v i,由下式计算第i个时间步上t i+1时刻的位移u i+1、速度
Figure PCTCN2020121713-appb-000007
和加速度ü i+1
Step-by-step calculation time, the end of each time step is calculated time displacements, velocity and acceleration for the i-th time step, known at time i t displacement velocity V i and u i, is calculated by the i Displacement u i+1 and velocity at t i+1 on two time steps
Figure PCTCN2020121713-appb-000007
And acceleration ü i+1 ;
1)选取迭代初始解:1) Select the initial solution of the iteration:
Figure PCTCN2020121713-appb-000008
Figure PCTCN2020121713-appb-000008
Figure PCTCN2020121713-appb-000009
Figure PCTCN2020121713-appb-000009
Figure PCTCN2020121713-appb-000010
Figure PCTCN2020121713-appb-000010
2)总共进行n次非线性迭代,n≥2,其中第k次迭代如下:2) A total of n non-linear iterations are performed, n≥2, and the kth iteration is as follows:
Figure PCTCN2020121713-appb-000011
Figure PCTCN2020121713-appb-000011
Figure PCTCN2020121713-appb-000012
Figure PCTCN2020121713-appb-000012
Figure PCTCN2020121713-appb-000013
Figure PCTCN2020121713-appb-000013
3)将第n次迭代结果作为目标解3) Take the result of the nth iteration as the target solution
Figure PCTCN2020121713-appb-000014
Figure PCTCN2020121713-appb-000014
Figure PCTCN2020121713-appb-000015
Figure PCTCN2020121713-appb-000015
Figure PCTCN2020121713-appb-000016
Figure PCTCN2020121713-appb-000016
优选地,γ取值范围为γ≥0.5。Preferably, the value range of γ is γ≥0.5.
优选地,γ取为0.5。Preferably, γ is taken as 0.5.
优选地,β取值范围为β≥0.25。Preferably, the value range of β is β≥0.25.
优选地,β取为0.25。Preferably, β is taken as 0.25.
优选地,σ取值范围为σ≥1。Preferably, the value range of σ is σ≥1.
优选地,σ取为1。Preferably, σ is taken as 1.
优选地,时间步长Δt取为基底输入加速度记录ü g的时间间隔的N倍,N为正整数,优选为1。 Preferably, the time step Δt is taken as N times the time interval of the base input acceleration record ü g , and N is a positive integer, preferably 1.
优选地,初始位移和初始速度均为0,即u 0=0且
Figure PCTCN2020121713-appb-000017
初始加速度ü 0=-ü g(0)。
Preferably, the initial displacement and initial velocity are both 0, that is, u 0 =0 and
Figure PCTCN2020121713-appb-000017
The initial acceleration ü 0 =-ü g (0).
优选地,所述n次非线性迭代中n取2。Preferably, n takes 2 in the n non-linear iterations.
本发明与现有技术相比,优点在于:Compared with the prior art, the present invention has the advantages of:
1)本发明的快速动力时程分析方法仅使用初始刚度矩阵K 0,而无需切线刚度矩阵K T,故不必更新等效刚度矩阵,只需在逐时间步计算之前,对等效刚度矩阵
Figure PCTCN2020121713-appb-000018
进行一次三角分解即可,避免了传统方法在每个时间步上重新计算并分解等效刚度矩阵的大量计算。
1) The fast dynamic time history analysis method of the present invention only uses the initial stiffness matrix K 0 and does not need the tangent stiffness matrix K T. Therefore, it is not necessary to update the equivalent stiffness matrix. It is only necessary to calculate the equivalent stiffness matrix before the time step calculation.
Figure PCTCN2020121713-appb-000018
Triangular decomposition can be performed once, which avoids the traditional method of recalculating and decomposing a large number of calculations of the equivalent stiffness matrix at each time step.
2)本发明采用了初始刚度矩阵放大系数σ,对含有特别硬化材料的结构,以及考虑几何非线性结构的,可通过选用σ≥1的值来保证算法的无条件稳定性。2) The present invention adopts the initial stiffness matrix amplification factor σ. For structures containing special hardened materials and considering geometrically nonlinear structures, the value of σ≥1 can be selected to ensure the unconditional stability of the algorithm.
3)本发明的快速动力时程分析方法在每个时间步上仅需进行固定次数的非线性迭代,一般2次即可,避免了传统方法迭代至满足容差所耗费的巨大计算量。3) The fast dynamic time history analysis method of the present invention only needs to perform a fixed number of nonlinear iterations at each time step, generally two times, which avoids the huge amount of calculation consumed by the traditional method to iterate to meet the tolerance.
4)本发明的快速动力时程分析方法具有2阶精度,与传统Newmark法精度相当。4) The fast dynamic time history analysis method of the present invention has a second-order accuracy, which is equivalent to the accuracy of the traditional Newmark method.
5)本发明的动力时程分析方法步骤简单,仅需对传统Newmark法的等效刚度更新机制进行改造,且对迭代次数进行限制,甚至无需编制新的程序,极易推广应用。5) The dynamic time history analysis method of the present invention has simple steps, only needs to modify the equivalent stiffness update mechanism of the traditional Newmark method, and restricts the number of iterations, even without the need to prepare a new program, and is easy to popularize and apply.
附图说明Description of the drawings
图1复杂高层结构示意图;Figure 1 Schematic diagram of complex high-rise structure;
图2 El-Centro波示意图;Figure 2 Schematic diagram of El-Centro wave;
图3 Newmark法和本发明动力时程分析方法计算的楼顶水平x方向位移对比示意图;Fig. 3 A comparison schematic diagram of the horizontal x-direction displacement of the roof calculated by the Newmark method and the dynamic time history analysis method of the present invention;
图4 Newmark法和本发明动力时程分析方法计算的楼顶水平x方向速度对比示意图;Fig. 4 A comparison schematic diagram of the horizontal x-direction velocity on the roof of a building calculated by the Newmark method and the dynamic time history analysis method of the present invention;
图5 Newmark法和本发明动力时程分析方法计算的楼顶竖直x方向加速度对比示意图;Fig. 5 A comparison schematic diagram of the vertical x-direction acceleration on the roof of a building calculated by the Newmark method and the dynamic time history analysis method of the present invention;
具体实施方式Detailed ways
下面结合具体实施例来对本发明进行进一步说明,但并不将本发明局限于这些具体实施方式。本领域技术人员应该认识到,本发明涵盖了权利要求书范围内所可能包括的所有备选方案、改进方案和等效方案。The present invention will be further described below in conjunction with specific examples, but the present invention is not limited to these specific embodiments. Those skilled in the art should realize that the present invention covers all alternatives, improvements and equivalents that may be included in the scope of the claims.
下面结合附图对本发明的结构原理和工作原理作具体的描述:The structural principle and working principle of the present invention will be described in detail below in conjunction with the accompanying drawings:
以一个复杂高层结构为实例,具体阐述本发明的非线性快速动力时程分析方法,复杂高层建筑如图1所示,该模型的前三个周期分别是T 1=1.815s,T 2=1.579s和T 3=0.890s。所述动力时程分析方法包含如下步骤: Taking a complex high-rise structure as an example, the nonlinear fast dynamic time history analysis method of the present invention is described in detail. The complex high-rise building is shown in Figure 1. The first three periods of the model are T 1 =1.815s and T 2 =1.579. s and T 3 =0.890s. The dynamic time history analysis method includes the following steps:
第一步,对所述高层建筑进行空间有限元离散,建立该建筑结构的有限元模型离散系统;所述高层建筑包括23945个节点,由8244个钢筋混凝土构件定义的9744个纤维梁单元和由177个剪力墙构件定义的4704个分层壳单元;梁柱采用纤维梁模型,剪力墙和楼板采用分层壳单元,并采用Rayleigh阻尼建立单元阻尼矩阵,由单元刚度矩阵、单元质量矩阵和单元阻尼矩阵集成整体刚度矩阵、整体质量矩阵和整体阻尼矩阵,并由Hamilton原理导出离散系统的运动方程组,建立离散系统的运动方程组:The first step is to carry out spatial finite element discretization of the high-rise building to establish a finite element model discrete system of the building structure; the high-rise building includes 23945 nodes, 9744 fiber beam elements defined by 8244 reinforced concrete members and 4704 layered shell elements defined by 177 shear wall components; fiber beam models are used for beams and columns, layered shell elements are used for shear walls and floor slabs, and Rayleigh damping is used to establish element damping matrix, which is composed of element stiffness matrix and element mass matrix The overall stiffness matrix, overall mass matrix and overall damping matrix are integrated with the element damping matrix, and the motion equations of the discrete system are derived from the Hamilton principle, and the motion equations of the discrete system are established:
Figure PCTCN2020121713-appb-000019
Figure PCTCN2020121713-appb-000019
其中,u,
Figure PCTCN2020121713-appb-000020
和ü分别为有限元模型各质点的位移,速度,加速度向量。M为质量矩阵,C为阻尼矩阵,F S为非线性回复力,是位移向量的非线性函数。P为外部动力荷载,如为地震作用时,P=-Mü g,ü g为建筑结构基底输入的地震动加速度,本例中,ü g采用如图2所示的El Centro地震波,该地震波的加速度记录间隔为0.01s,分析步长采用Δt=0.01s。该步空间有限元法的离散过程为广泛应用的常规操作,细节不在此赘述。计算阻尼矩阵C时,采用5%的阻尼比,选择第1和第9模态来计算瑞利阻尼系数,包括质量阻尼和初始刚度比例阻尼。
Where u,
Figure PCTCN2020121713-appb-000020
And ü are the displacement, velocity and acceleration vectors of each particle of the finite element model. M is the mass matrix, C is the damping matrix, and F S is the nonlinear restoring force, which is the nonlinear function of the displacement vector. P is the external dynamic load. If it is an earthquake, P=-Mü g , ü g is the ground motion acceleration input from the base of the building structure. In this example, ü g uses the El Centro seismic wave shown in Figure 2. The acceleration recording interval is 0.01s, and the analysis step length is Δt=0.01s. The discrete process of this step space finite element method is a widely used routine operation, and the details will not be repeated here. When calculating the damping matrix C, a damping ratio of 5% is used, and the first and ninth modes are selected to calculate the Rayleigh damping coefficient, including mass damping and initial stiffness proportional damping.
第二步,选取参数和确定全局不变量:The second step is to select parameters and determine global invariants:
1)选取γ、β、σ1) Select γ, β, σ
γ取值范围为γ≥0.5,一般取为0.5;The value range of γ is γ≥0.5, generally 0.5;
β取值范围为β≥0.25,一般取为0.25;The value range of β is β≥0.25, generally 0.25;
σ取值范围为σ≥1,一般取为1;The value range of σ is σ≥1, and it is generally 1;
本实施例中,参数选取为γ=0.5,β=0.25,σ=1;In this embodiment, the parameters are selected as γ=0.5, β=0.25, and σ=1;
2)选取时间步长Δt,一般取为基底输入加速度记录ü g的时间间隔的N倍,N一般等于1,本实施例中,在基底输入如图2所示的El Centro地震波,该地震波的加速度记录间隔为0.01s,分析步长采用Δt=0.01s; 2) Select the time step Δt, which is generally N times the time interval of the base input acceleration record ü g , and N is generally equal to 1. In this embodiment, the El Centro seismic wave shown in Figure 2 is input into the base. The acceleration recording interval is 0.01s, and the analysis step length is Δt=0.01s;
3)根据已知的初始位移u 0和初始速度
Figure PCTCN2020121713-appb-000021
确定初始加速度ü 0
3) According to the known initial displacement u 0 and initial velocity
Figure PCTCN2020121713-appb-000021
Determine the initial acceleration ü 0 ;
Figure PCTCN2020121713-appb-000022
Figure PCTCN2020121713-appb-000022
本实施例中,初始位移和初始速度均为0,即u 0=0且
Figure PCTCN2020121713-appb-000023
故初始加速度ü 0=-ü g(0);
In this embodiment, the initial displacement and initial velocity are both 0, that is, u 0 =0 and
Figure PCTCN2020121713-appb-000023
So the initial acceleration ü 0 =-ü g (0);
4)计算等效刚度矩阵
Figure PCTCN2020121713-appb-000024
4) Calculate the equivalent stiffness matrix
Figure PCTCN2020121713-appb-000024
Figure PCTCN2020121713-appb-000025
Figure PCTCN2020121713-appb-000025
其中,K 0为非线性回复力F S(u)在u 0处雅可比矩阵,即初始刚度矩阵。 Among them, K 0 is the Jacobian matrix of the nonlinear restoring force F S (u) at u 0 , that is, the initial stiffness matrix.
第三步,逐时间步计算,计算每个时间步结束时刻的位移、速度和加速度,对于第i个时间步,已知t i时刻的位移u i和速度v i,由下式计算第i个时间步上t i+1时刻的位移u i+1、速度
Figure PCTCN2020121713-appb-000026
和加速度ü i+1
Step-by-step calculation time, the end of each time step is calculated time displacements, velocity and acceleration for the i-th time step, known at time i t displacement velocity V i and u i, is calculated by the i Displacement u i+1 and velocity at t i+1 on two time steps
Figure PCTCN2020121713-appb-000026
And acceleration ü i+1 ;
1)选取迭代初始解:1) Select the initial solution of the iteration:
Figure PCTCN2020121713-appb-000027
Figure PCTCN2020121713-appb-000027
Figure PCTCN2020121713-appb-000028
Figure PCTCN2020121713-appb-000028
Figure PCTCN2020121713-appb-000029
Figure PCTCN2020121713-appb-000029
2)总共进行n次非线性迭代,n≥2,一般取2,其中第k次迭代如下:2) A total of n non-linear iterations are performed, n≥2, generally 2, where the kth iteration is as follows:
Figure PCTCN2020121713-appb-000030
Figure PCTCN2020121713-appb-000030
Figure PCTCN2020121713-appb-000031
Figure PCTCN2020121713-appb-000031
Figure PCTCN2020121713-appb-000032
Figure PCTCN2020121713-appb-000032
3)将第n次迭代结果作为目标解3) Take the result of the nth iteration as the target solution
Figure PCTCN2020121713-appb-000033
Figure PCTCN2020121713-appb-000033
Figure PCTCN2020121713-appb-000034
Figure PCTCN2020121713-appb-000034
Figure PCTCN2020121713-appb-000035
Figure PCTCN2020121713-appb-000035
为了展示本发明的动力时程分析方法高效性和精确性,比较例采用最常用的二阶精度Newmark法进行分析,为方便对比,Newark法的参数同样选为,γ=0.5,β=0.25,步长采用Δt=0.01s,非线性迭代收敛容差选为Tol=0.001,分析结果如图3-5所示,计算耗费时间为300小时。而采用本发明的动力时程分析方法,其结果和采用Newmark法的结果非常接近(2条响应曲线几乎重合),具体结果如图3-5所示。然而采用本发明方法的计算时间仅为5小时,本发明的动力时程分析方法在保证计算效率的前提下,大幅减少了计算工作量,将计算效率提升了60倍。In order to demonstrate the efficiency and accuracy of the dynamic time history analysis method of the present invention, the comparative example adopts the most commonly used second-order precision Newmark method for analysis. For the convenience of comparison, the parameters of the Newark method are also selected as γ=0.5, β=0.25, The step size is Δt=0.01s, and the nonlinear iterative convergence tolerance is selected as Tol=0.001. The analysis result is shown in Figure 3-5. The calculation time is 300 hours. With the dynamic time history analysis method of the present invention, the result is very close to the result using the Newmark method (the two response curves almost overlap), and the specific results are shown in Figures 3-5. However, the calculation time using the method of the present invention is only 5 hours. Under the premise of ensuring the calculation efficiency, the dynamic time history analysis method of the present invention greatly reduces the calculation workload and increases the calculation efficiency by 60 times.
从实施例中可以看到,本发明的快速动力时程分析方法具备如下优点:It can be seen from the embodiments that the fast power time history analysis method of the present invention has the following advantages:
1)本发明的快速动力时程分析方法仅使用初始刚度矩阵K 0,而无需切线刚度矩阵K T,故不必更新等效刚度矩阵,只需在逐时间步计算之前,对等效刚度矩阵
Figure PCTCN2020121713-appb-000036
进行一次三角分解即可,避免了传统方法在每个时间步上重新计算并分解等效刚度矩阵的大量计算。
1) The fast dynamic time history analysis method of the present invention only uses the initial stiffness matrix K 0 and does not need the tangent stiffness matrix K T. Therefore, it is not necessary to update the equivalent stiffness matrix. It is only necessary to calculate the equivalent stiffness matrix before the time step calculation.
Figure PCTCN2020121713-appb-000036
Triangular decomposition can be performed once, which avoids the traditional method of recalculating and decomposing a large number of calculations of the equivalent stiffness matrix at each time step.
2)本发明采用了初始刚度矩阵放大系数σ,对含有特别硬化材料的结构,以及考虑几何非线性结构的,可通过选用σ≥1的值来保证算法的无条件稳定性。2) The present invention adopts the initial stiffness matrix amplification factor σ. For structures containing special hardened materials and considering geometrically nonlinear structures, the value of σ≥1 can be selected to ensure the unconditional stability of the algorithm.
3)本发明的快速动力时程分析方法在每个时间步上仅需进行固定次数的非线性迭代,一般2次即可,避免了传统方法迭代至满足容差所耗费的巨大计算量。3) The fast dynamic time history analysis method of the present invention only needs to perform a fixed number of nonlinear iterations at each time step, generally two times, which avoids the huge amount of calculation consumed by the traditional method to iterate to meet the tolerance.
4)本发明的快速动力时程分析方法具有2阶精度,与传统Newmark法精度相当。4) The fast dynamic time history analysis method of the present invention has a second-order accuracy, which is equivalent to the accuracy of the traditional Newmark method.
5)本发明的动力时程分析方法步骤简单,仅需对传统Newmark法的等效刚度更新机制进行改造,且对迭代次数进行限制,甚至无需编制新的程序,极易推广应用。5) The dynamic time history analysis method of the present invention has simple steps, only needs to modify the equivalent stiffness update mechanism of the traditional Newmark method, and restricts the number of iterations, even without the need to prepare a new program, and is easy to popularize and apply.
应当理解的是,本发明描述的方法的步骤仅仅是示例性的描述,对其先后进行的时间顺序没有特殊的要求,除非其本身有必然的先后顺序关系。It should be understood that the steps of the method described in the present invention are only exemplary descriptions, and there is no special requirement on the time sequence of their sequential execution, unless they have a certain sequence relationship.
如上所示,本发明虽然已参照有限的实施例和附图进行了说明,但在本发明所属领域中具备通常知识的人均可以从此记载中进行各种修改和变形。由此,其他实施例及权利要求书与等同物均属于权利要求的保护范围。As shown above, although the present invention has been described with reference to limited embodiments and drawings, anyone with ordinary knowledge in the field to which the present invention pertains can make various modifications and variations from this description. Therefore, other embodiments, claims, and equivalents fall within the protection scope of the claims.

Claims (10)

  1. 一种复杂建筑结构非线性动力时程分析方法,所述方法是一种用于外部动力荷载作用下复杂建筑结构非线性动力时程分析的固定迭代次数分析方法,其步骤如下:A nonlinear dynamic time history analysis method for complex building structures. The method is a fixed iteration number analysis method for nonlinear dynamic time history analysis of complex building structures under external dynamic loads. The steps are as follows:
    第一步,对所述复杂建筑结构进行空间有限元离散,建立该建筑结构的有限元模型离散系统,梁柱采用纤维梁模型,剪力墙和楼板采用分层壳单元,并采用Rayleigh阻尼建立单元阻尼矩阵,由单元刚度矩阵、单元质量矩阵和单元阻尼矩阵集成整体刚度矩阵、整体质量矩阵和整体阻尼矩阵,并由Hamilton原理导出离散系统的运动方程组,建立离散系统的运动方程组:The first step is to perform spatial finite element discretization of the complex building structure, and establish a finite element model discrete system for the building structure. The beams and columns adopt fiber beam models, and the shear walls and floor slabs adopt layered shell elements and Rayleigh damping. The element damping matrix integrates the overall stiffness matrix, the overall mass matrix and the overall damping matrix by the element stiffness matrix, the element mass matrix and the element damping matrix, and the motion equations of the discrete system are derived from the Hamilton principle, and the motion equations of the discrete system are established:
    Figure PCTCN2020121713-appb-100001
    Figure PCTCN2020121713-appb-100001
    其中,u,
    Figure PCTCN2020121713-appb-100002
    Figure PCTCN2020121713-appb-100003
    分别为有限元模型各质点的位移,速度,加速度向量;M为质量矩阵,C为阻尼矩阵,F S为非线性回复力,是位移向量的非线性函数;P为外部动力荷载,地震作用时,
    Figure PCTCN2020121713-appb-100004
    Figure PCTCN2020121713-appb-100005
    为建筑结构基底输入的地震动加速度;
    Where u,
    Figure PCTCN2020121713-appb-100002
    with
    Figure PCTCN2020121713-appb-100003
    They are the displacement, velocity, and acceleration vectors of each particle of the finite element model; M is the mass matrix, C is the damping matrix, and F S is the nonlinear restoring force, which is a nonlinear function of the displacement vector; P is the external dynamic load, during earthquake action ,
    Figure PCTCN2020121713-appb-100004
    Figure PCTCN2020121713-appb-100005
    Ground motion acceleration input for the base of the building structure;
    第二步,选取参数和确定全局不变量:The second step is to select parameters and determine global invariants:
    1)选取γ、β、σ;1) Select γ, β, σ;
    2)选取时间步长Δt;2) Select the time step Δt;
    3)根据已知的初始位移u 0和初始速度
    Figure PCTCN2020121713-appb-100006
    确定初始加速度
    Figure PCTCN2020121713-appb-100007
    3) According to the known initial displacement u 0 and initial velocity
    Figure PCTCN2020121713-appb-100006
    Determine the initial acceleration
    Figure PCTCN2020121713-appb-100007
    Figure PCTCN2020121713-appb-100008
    Figure PCTCN2020121713-appb-100008
    4)计算等效刚度矩阵
    Figure PCTCN2020121713-appb-100009
    4) Calculate the equivalent stiffness matrix
    Figure PCTCN2020121713-appb-100009
    Figure PCTCN2020121713-appb-100010
    Figure PCTCN2020121713-appb-100010
    其中,K 0为非线性回复力F S(u)在u 0处雅可比矩阵,即初始刚度矩阵; Among them, K 0 is the Jacobian matrix of the nonlinear restoring force F S (u) at u 0 , that is, the initial stiffness matrix;
    第三步,逐时间步计算,计算每个时间步结束时刻的位移、速度和加速度,对于第i个时间步,已知t i时刻的位移u i和速度v i,由下式计算第i个时间步上t i+1时刻的位移u i+1、速度
    Figure PCTCN2020121713-appb-100011
    和加速度
    Figure PCTCN2020121713-appb-100012
    Step-by-step calculation time, the end of each time step is calculated time displacements, velocity and acceleration for the i-th time step, known at time i t displacement velocity V i and u i, is calculated by the i Displacement u i+1 and velocity at t i+1 on two time steps
    Figure PCTCN2020121713-appb-100011
    And acceleration
    Figure PCTCN2020121713-appb-100012
    1)选取迭代初始解:1) Select the initial solution of the iteration:
    Figure PCTCN2020121713-appb-100013
    Figure PCTCN2020121713-appb-100013
    Figure PCTCN2020121713-appb-100014
    Figure PCTCN2020121713-appb-100014
    Figure PCTCN2020121713-appb-100015
    Figure PCTCN2020121713-appb-100015
    2)总共进行n次非线性迭代,n≥2,其中第k次迭代如下:2) A total of n non-linear iterations are performed, n≥2, and the kth iteration is as follows:
    Figure PCTCN2020121713-appb-100016
    Figure PCTCN2020121713-appb-100016
    Figure PCTCN2020121713-appb-100017
    Figure PCTCN2020121713-appb-100017
    Figure PCTCN2020121713-appb-100018
    Figure PCTCN2020121713-appb-100018
    3)将第n次迭代结果作为目标解3) Take the result of the nth iteration as the target solution
    Figure PCTCN2020121713-appb-100019
    Figure PCTCN2020121713-appb-100019
    Figure PCTCN2020121713-appb-100020
    Figure PCTCN2020121713-appb-100020
    Figure PCTCN2020121713-appb-100021
    Figure PCTCN2020121713-appb-100021
  2. 根据权利要求1所述的复杂建筑结构非线性动力时程分析方法,其特征在于,γ取值范围为γ≥0.5。The nonlinear dynamic time history analysis method of a complex building structure according to claim 1, wherein the value range of γ is γ≥0.5.
  3. 根据权利要求2所述的复杂建筑结构非线性动力时程分析方法,其特征在于,γ取为0.5。The nonlinear dynamic time history analysis method of a complex building structure according to claim 2, wherein γ is taken as 0.5.
  4. 根据权利要求1所述的复杂建筑结构非线性动力时程分析方法,其特征在于,β取值范围为β≥0.25。The nonlinear dynamic time history analysis method of a complex building structure according to claim 1, wherein the value range of β is β≥0.25.
  5. 根据权利要求4所述的复杂建筑结构非线性动力时程分析方法,其特征在于,β取为0.25。The nonlinear dynamic time history analysis method of a complex building structure according to claim 4, wherein β is taken as 0.25.
  6. 根据权利要求1所述的复杂建筑结构非线性动力时程分析方法,其特征在于,σ取值范围为σ≥1。The nonlinear dynamic time history analysis method of a complex building structure according to claim 1, wherein the value range of σ is σ≥1.
  7. 根据权利要求6所述的复杂建筑结构非线性动力时程分析方法,其特征在于,σ取为1。The nonlinear dynamic time history analysis method of a complex building structure according to claim 6, wherein σ is taken as 1.
  8. 根据权利要求1-7任一项所述的复杂建筑结构非线性动力时程分析方法,其特征在于,时间步长Δt取为基底输入加速度记录
    Figure PCTCN2020121713-appb-100022
    的时间间隔的N倍,N为正整数。
    The nonlinear dynamic time history analysis method of a complex building structure according to any one of claims 1-7, wherein the time step Δt is taken as the base input acceleration record
    Figure PCTCN2020121713-appb-100022
    The time interval is N times, and N is a positive integer.
  9. 根据权利要求1-8所述的复杂建筑结构非线性动力时程分析方法,其特征在于,初始位移和初始速度均为0,即u 0=0且
    Figure PCTCN2020121713-appb-100023
    初始加速度
    Figure PCTCN2020121713-appb-100024
    The nonlinear dynamic time history analysis method for complex building structures according to claims 1-8, wherein the initial displacement and initial velocity are both 0, that is, u 0 =0 and
    Figure PCTCN2020121713-appb-100023
    Initial acceleration
    Figure PCTCN2020121713-appb-100024
  10. 根据权利要求1-9任一项所述的复杂建筑结构非线性动力时程分析方法,其特征在于,所述n次非线性迭代中n取2。The nonlinear dynamic time history analysis method of a complex building structure according to any one of claims 1-9, wherein n is 2 in the n-th nonlinear iteration.
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