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  4. 2005
Showing papers on "Newmark-beta method published in 2005"
Journal Article•10.2514/1.27606•
Nonlinear Flight Dynamics of Very Flexible Aircraft

[...]

Christopher M. Shearer1, Christopher M. Shearer2, Carlos E. S. Cesnik•
Air Force Institute of Technology1, University of Michigan2
15 Aug 2005-Journal of Aircraft
TL;DR: In this paper, a low-order strain-based nonlinear structural analysis coupled with unsteady flnite-state potential ∞ow aerodynamics form the basis for the aeroelastic model.
Abstract: This paper focuses on the characterization of the response of a very ∞exible aircraft in ∞ight. The 6-DOF equations of motion of a reference point on the aircraft are coupled with the aeroelastic equations that govern the geometrically nonlinear structural response of the vehicle. A low-order strain-based nonlinear structural analysis coupled with unsteady flnite-state potential ∞ow aerodynamics form the basis for the aeroelastic model. The nonlinear beam structural model assumes constant strain over an element in extension, twist, and in/out of plane bending. The geometrically nonlinear structural formulation, the flnite state aerodynamic model, and the nonlinear rigid body equations together provide a low-order complete nonlinear aircraft analysis tool. The equations of motion are integrated using an implicit modifled generalized-alpha method. The method incorporates both flrst and second order nonlinear equations without the necessity of transforming the equations to flrst order and incorporates a Newton-Raphson sub-iteration scheme at each time step. Using the developed tool, analyses and simulations can be conducted which encompass nonlinear rigid body, nonlinear rigid body coupled with linearized structural solutions, and full nonlinear rigid body and structural solutions. Simulations are presented which highlight the importance of nonlinear structural modeling as compared to rigid body and linearized structural analyses in a representative High Altitude Long Endurance (HALE) vehicle. Results show signiflcant difierences in the three reference point axes (pitch, roll, and yaw) not previously captured by linearized or rigid body approaches. The simulations using both full and empty fuel states include level gliding descent, low-pass flltered square aileron input rolling/gliding descent, and low-pass square elevator input gliding descent. Results are compared for rigid body, linearized structural, and nonlinear structural response.

314 citations

Journal Article•10.1007/S00466-004-0630-9•
A remark on the application of the Newton-Raphson method in non-linear finite element analysis

[...]

Stefan Hartmann1•
University of Kassel1
14 Apr 2005-Computational Mechanics
TL;DR: In this paper, the effects of a consistent application of the classical Newton-Raphson method in connection with the finite element method, and compare it with the classical multilevel-Newton algorithm is applied.
Abstract: Usually the notion “Newton-Raphson method” is used in the context of non-linear finite element analysis based on quasi-static problems in solid mechanics. It is pointed out that this is only true in the case of non-linear elasticity. In the case of constitutive equations of evolutionary-type, like in viscoelasticity, viscoplasticity or elastoplasticity, the “Multilevel-Newton algorithm” is usually applied yielding the notions of global and local level (iteration), as well as the consistent tangent operator. In this paper, we investigate the effects of a consistent application of the classical Newton-Raphson method in connection with the finite element method, and compare it with the classical Multilevel-Newton algorithm. Furthermore, an improved version of the Multilevel-Newton method is applied.

101 citations

Journal Article•10.1002/NME.1368•
A combined space–time extended finite element method

[...]

Julien Réthoré1, Anthony Gravouil1, Alain Combescure1•
Institut national des sciences Appliquées de Lyon1
14 Sep 2005-International Journal for Numerical Methods in Engineering
TL;DR: In this paper, an enriched basis of shape functions in time is used to capture with a good accuracy the non-polynomial part of the solution, which allows a suitable form of the time-stepping formulae to study stability and energy conservation.
Abstract: The Newmark method for the numerical integration of second order equations has been extensively used and studied along the past fifty years for structural dynamics and various fields of mechanical engineering. Easy implementation and nice properties of this method and its derivatives for linear problems are appreciated but the main drawback is the treatment of discontinuities. Zienkiewicz proposed an approach using finite element concept in time, which allows a new look at the Newmark method. The idea of this paper is to propose, thanks to this approach, the use of a time partition of the unity method denoted Time Extended Finite Element Method (TX-FEM) for improved numerical simulations of time discontinuities. An enriched basis of shape functions in time is used to capture with a good accuracy the non-polynomial part of the solution. This formulation allows a suitable form of the time-stepping formulae to study stability and energy conservation. The case of an enrichment with the Heaviside function is developed and can be seen as an alternative approach to time discontinuous Galerkin method (T-DGM), stability and accuracy properties of which can be derived from those of the TX-FEM. Then Space and Time X-FEM (STX-FEM) are combined to obtain a unified space–time discretization. This combined STX-FEM appears to be a suitable technique for space–time discontinuous problems like dynamic crack propagation or other applications involving moving discontinuities. Copyright © 2005 John Wiley & Sons, Ltd.

68 citations

Journal Article•10.1016/J.JSV.2004.09.010•
The effect of temperature on the large amplitude vibrations of curved beams

[...]

Pedro Ribeiro1, Emil Manoach2•
University of Porto1, Bulgarian Academy of Sciences2
06 Aug 2005-Journal of Sound and Vibration
TL;DR: In this paper, the influence of parameters like the temperature variation, the thickness and the ratio of curvature on the beams nonlinear dynamics is studied and the nonlinear equations of motion are solved in the time domain by Newmark's method.

56 citations

Journal Article•10.1016/J.AMC.2003.12.102•
Numerical solution of damped nonlinear Klein-Gordon equations using variational method and finite element approach

[...]

Quan-Fang Wang1, Daizhan Cheng1•
Chinese Academy of Sciences1
01 Mar 2005-Applied Mathematics and Computation
TL;DR: Numerical treatment for damped nonlinear Klein-Gordon equations, based on variational method and finite element approach, is studied and a semi-discrete algorithm is proposed by using quadratic interpolation functions of continuous time and spatial dimension one.

51 citations

Journal Article•10.1016/J.COMPSTRUCT.2005.09.009•
Active control of forced vibrations in adaptive structures using a higher order model

[...]

José Mateus Simões Moita1, Cristóvão M. Mota Soares2, Carlos A. Mota Soares2•
University of the Algarve1, Instituto Superior Técnico2
01 Dec 2005-Composite Structures
TL;DR: In this article, a finite element formulation for active control of forced vibrations, including resonance, of thin plate/shell laminated structures with integrated piezoelectric layers, acting as sensors and actuators, based on third-order shear deformation theory, is presented.

45 citations

Journal Article•10.1016/J.JSV.2004.06.026•
Aerodynamic and aeroelastic analysis of bundled cables by numerical simulation

[...]

Alexandre Luis Braun1, Armando Miguel Awruch1•
Universidade Federal do Rio Grande do Sul1
07 Jun 2005-Journal of Sound and Vibration
TL;DR: In this article, a numerical model for the aerodynamic and aeroelastic analysis of bundled cables, commonly used in energy transmission lines, is presented, where the bundles were idealized by a sectional model representing the section at the mid span between two supporting towers.

42 citations

Journal Article•10.1002/EQE.425•
Modified predictor–corrector numerical scheme for real‐time pseudo dynamic tests using state‐space formulation

[...]

Yunfeng Zhang1, Richard Sause1, James M. Ricles1, Clay Naito1•
Lehigh University1
01 Mar 2005-Earthquake Engineering & Structural Dynamics
TL;DR: In this article, an explicit numerical integration method for real-time dynamic tests is proposed, termed the MPC-SSP method, which is suited to use in real- time pseudo dynamic tests as no iteration steps are involved in each step of computation.
Abstract: This paper deals with an explicit numerical integration method for real-time pseudo dynamic tests. The proposed method, termed the MPC-SSP method, is suited to use in real-time pseudo dynamic tests as no iteration steps are involved in each step of computation. A procedure for implementing the proposed method in real-time pseudo dynamic tests is described in the paper. A state-space approach is employed in this study to formulate the equations of motion of the system, which is advantageous in real-time pseudo dynamic testing of structures with active control devices since most structural control problems are formulated in state space. A stability and accuracy analysis of the proposed method was performed based on linear elastic systems. Owing to an extrapolation scheme employed to predict the system's future response, the MPC-SSP method is conditionally stable. To demonstrate the effectiveness of the MPC-SSP method, a series of numerical simulations were performed and the performance of the MPC-SSP method was compared with other pseudo dynamic testing methods including Explicit Newmark, Central Difference, Operator Splitting, and OS-SSP methods based on both linear and non-linear single-degree-of-freedom systems. Copyright © 2004 John Wiley & Sons, Ltd.

38 citations

Journal Article•10.1007/S00466-005-0663-8•
The bi-potential method applied to the modeling of dynamic problems with friction

[...]

Zhi-Qiang Feng1, Pierre Joli1, Jean-Michel Cros1, Benoit Magnain1•
University of Évry Val d'Essonne1
14 Jul 2005-Computational Mechanics
TL;DR: In this paper, a first-order algorithm is applied to the numerical integration of the time-discretized equation of motion, and a finite element code including pre/postprocessor FER/Impact is developed.
Abstract: The bi-potential method has been successfully applied to the modeling of frictional contact problems in static cases. This paper presents an extension of this method for dynamic analysis of impact problems with deformable bodies. A first order algorithm is applied to the numerical integration of the time-discretized equation of motion. Using the Object-Oriented Programming (OOP) techniques in C++ and OpenGL graphical support, a finite element code including pre/postprocessor FER/Impact is developed. The numerical results show that, at the present stage of development, this approach is robust and efficient in terms of numerical stability and precision compared with the penalty method.

32 citations

Journal Article•10.1002/NME.1331•
Adaptive superposition of finite element meshes in elastodynamic problems

[...]

Z. Yue1, D. H. Robbins1•
University of Maryland, College Park1
21 Jul 2005-International Journal for Numerical Methods in Engineering
TL;DR: In this article, an adaptive finite element procedure is developed for modeling transient phenomena in elastic solids, including both wave propagation and structural dynamics, using mesh superposition to produce spatial refinement (referred to as sadaptivity) in transient problems.
Abstract: An adaptive finite element procedure is developed for modelling transient phenomena in elastic solids, including both wave propagation and structural dynamics. Although both temporal and spatial adaptivity are addressed, the novel feature of the formulation is the use of mesh superposition to produce spatial refinement (referred to as s-adaptivity) in transient problems. Spatial error estimation is based on superconvergent patch recovery of higher-order accurate stresses and is used to guide mesh adaptivity, while the temporal error estimation is based on the assumption of linearly varying third-order time derivatives of the displacement field and is used to adjust the time step size for the HHT-α variant of the Newmark direct numerical integration method. Spatial adaptivity of the mesh is performed using a hierarchical h-refinement scheme that is efficiently implemented using a structured version of finite element mesh superposition. This particular spatial adaptivity scheme is extremely fast and consequently makes it feasible to repeatedly update both the mesh and the time increment as required in an adaptive transient analysis. This work represents the initial effort in applying this type of spatial adaptivity to transient problems. Three example problems are given to demonstrate the performance characteristics of the s-adaptive procedure. Copyright © 2005 John Wiley & Sons, Ltd.

32 citations

Journal Article•10.1109/LMWC.2005.859968•
Improving the Newmark time integration scheme in finite element time domain methods

[...]

Jr. W.A. Artuzi
05 Dec 2005-IEEE Microwave and Wireless Components Letters
TL;DR: In this paper, the Newmark formulation for the time-stepping solution of the electric field vector wave equation is modified in order to suppress low-frequency spurious responses, which has the advantage of halving the number of iterations necessary to solve the system of linear equations.
Abstract: The Newmark formulation for the time-stepping solution of the electric field vector wave equation is modified in order to suppress low-frequency spurious responses. It is verified that the proposed method has the advantage of halving the number of iterations necessary to solve the system of linear equations and it is shown that setting the number of iterations per time step can be more convenient than establishing a residual tolerance to verify convergence. In addition, the use of diagonal and incomplete Cholesky preconditioners are tested through numerical examples and they appear to be equivalent in terms of CPU time, leaving the first as the preferable choice concerning memory storage and programing facilities.
Proceedings Article•10.1115/IMECE2005-81770•
The Newmark Integration Method for Simulation of Multibody Systems: Analytical Considerations

[...]

B. Gavrea1, Dan Negrut2, Florian A. Potra1•
University of Maryland, Baltimore County1, Argonne National Laboratory2
1 Jan 2005
TL;DR: A new approach in which BDF methods are replaced by the Newmark formulas is proposed, which is implemented successfully for industrial strength Dynamic Analysis simulations in the 2005 version of the MSC.ADAMS software and used very effectively for the simulation of systems with more than 15,000 differential-algebraic equations.
Abstract: When simulating the behavior of a mechanical system, the time evolution of the generalized coordinates used to represent the configuration of the model is computed as the solution of a combined set of ordinary differential and algebraic equations (DAEs). There are several ways in which the numerical solution of the resulting index 3 DAE problem can be approached. The most well-known and time-honored algorithms are the direct discretization approach, and the state-space reduction approach, respectively. In the latter, the problem is reduced to a minimal set of potentially new generalized coordinates in which the problem assumes the form of a pure second order set of Ordinary Differential Equations (ODE). This approach is very accurate, but computationally intensive, especially when dealing with large mechanical systems that contain flexible parts, stiff components, and contact/impact. The direct discretization approach is less but nevertheless sufficiently accurate yet significantly faster, and it is the approach that is considered in this paper. In the context of direct discretization methods, approaches based on the Backward Differentiation Formulas (BDF) have been the traditional choice for more than 20 years. This paper proposes a new approach in which BDF methods are replaced by the Newmark formulas. Local convergence analysis is carried out for the proposed method, and step-size control, error estimation, and nonlinear system solution related issues are discussed in detail. A series of two simple models are used to validate the method. The global convergence analysis and a computational-efficiency comparison with the most widely used numerical integrator available in the MSC.ADAMS commercial simulation package are forthcoming. The new method has been implemented successfully for industrial strength Dynamic Analysis simulations in the 2005 version of the MSC.ADAMS software and used very effectively for the simulation of systems with more than 15,000 differential-algebraic equations.Copyright © 2005 by ASME
Book•
What Every Engineer Should Know About Computational Techniques of Finite Element Analysis

[...]

Louis Komzsik
1 Mar 2005
TL;DR: Nonlinear Analysis Introduction to Nonlinear Analysis Newton-Raphson Methods Quasi-Newton Iteration Techniques Convergence Criteria Computatory Example Nonlinear Dynamics Sensitivity and Optimization Design Sensitivity Design Optimization Planar Bending of the Bar Computational Example.
Abstract: NUMERICAL MODEL GENERATION Finite Element Analysis Solution of Boundary Value Problems Finite Element Shape Functions Finite Element Basis Functions Assembly of Finite Element Matrices Element Matrix Generation Local to Global Coordinate Transformation A Quadrilateral Finite Element References Finite Element Model Generation Spline Approximation Geometric Modeling Objects Geometric Model Discretization Delaunay Mesh Generation References Modeling of Physical Phenomena Lagrange's Equations of Motion Continuum Mechanical Systems Finite Element Analysis of Elastic Continuum A Tetrahedral Finite Element Equation of Motion of Mechanical System Transformation to Frequency Domain References Constraints and Boundary Conditions The Concept of Multi-Point Constraints The Elimination of Multi-Point Constraints The Axial Bar Element The Concept of Single Point Constraints The Elimination of Single Point Constraints References Singularity Detection of Finite Element Models Local Singularities Global Singularities Massless Degrees of Freedom Industrial Case Studies References COMPUTATIONAL REDUCTION TECHNIQUES Matrix Factorization and Linear System Solution Finite Element Matrix Reordering Sparse Matrix Factorization Multifrontal Factorization Linear System Solution Distributed Factorization and Solution Factorization Case Study References Static Condensation Single Level, Single Component Condensation Computational Example Single Level, Multiple Component Condensation Multiple Level Static Condensation Static Condensation Case Study References Spectral Computations Spectral Transformation Lanczos Reduction Generalized Eigenvalue Problem Eigenvalue Computation Distributed Eigenvalue Computation Normal Modes Analysis Case Study Complex Spectral Computations Complex Modes Analysis Case Study Dense Eigenvalue Analysis Householder Reduction Techniques Tridiagonal Reduction Reduction to Hessenberg Form References Dynamic Reduction Single Level, Single Component Dynamic Reduction Accuracy of Dynamic Reduction Computational Example Single Level, Multiple Component Dynamic Reduction Multiple Level Dynamic Reduction Multibody Analysis Application References Component Modal Synthesis Single Level, Single Component Modal Synthesis Mixed Boundary Component Mode Reduction Computational Example Single Level, Multiple Component Modal Synthesis Multiple Level Modal Synthesis Component Modal Synthesis Case Study References ENGINEERING SOLUTION COMPUTATIONS Modal Solution Technique Modal Reduction Truncation Error in Modal Reduction The Method of Residual Flexibility The Method of Mode Acceleration Coupled Modal Solution Application References Transient Response Analysis The Central Difference Method The Newmark Method Starting Conditions and Time Step Changes Stability of Time Integration Techniques Transient Solution Case Study References Frequency Domain Analysis Direct Frequency Response Analysis Reduced Order Frequency Response Analysis Accuracy of Reduced Order Solution Frequency Response Case Study References Nonlinear Analysis Introduction to Nonlinear Analysis Newton-Raphson Methods Quasi-Newton Iteration Techniques Convergence Criteria Computational Example Nonlinear Dynamics References Sensitivity and Optimization Design Sensitivity Design Optimization Planar Bending of the Bar Computational Example Eigenfunction Sensitivities Variational Analysis References Engineering Result Computations Displacement Recovery Stress Calculation Nodal Data Interpolation Level Curve Computation Engineering Results Case Study References Closing Remarks Annotation Index
Journal Article•10.1016/J.CMA.2004.11.010•
Explorations of a family of stochastic Newmark methods in engineering dynamics

[...]

Debasish Roy1, M.K. Dash2•
Indian Institute of Science1, Indira Gandhi Institute of Technology2
01 Nov 2005-Computer Methods in Applied Mechanics and Engineering
TL;DR: In this paper, a family of stochastic Newmark maps are explored for direct integrations of linear dynamical systems of engineering interest, where the response variables are assumed to be modeled by white noise processes or their filters and may be applied additively or multiplicatively.
Journal Article•10.1002/NME.1268•
Vibration analyses of a portal frame under the action of a moving distributed mass using moving mass element

[...]

Jia-Jang Wu1•
National Kaohsiung Marine University1
14 Apr 2005-International Journal for Numerical Methods in Engineering
TL;DR: In this paper, four kinds of moving mass elements, 1st-node, 2nd-node and full and short-range mass elements are presented, where the full mass element refers to that with mass distributed from the first node (or second node) to the arbitrary position of a two-node beam element, while the short range mass element is the case with its location arbitrary on a beam element.
Abstract: Four kinds of moving mass elements, 1st-node, 2nd-node, full and short-range mass elements, are presented, where the 1st-node (or 2nd-node) mass element refers to that with mass distributed from the first node (or second node) to the arbitrary position of a two-node beam element, the full mass element is the special case of the 1st-node (or 2nd-node) mass element with mass distributed over the full length of the beam element, while the short-range mass element is the case with its location arbitrary on a beam element. If the total range of a distributed mass is denoted by R and the length of each beam element is denoted by , then, for the case of R≥, one may model the distributed mass on the beam using the combination of the 1st-node, 2nd-node and full mass elements, while for the case of R <, one may model the distributed mass using the short-range mass element. It has been found that the effects of the vertical (y) and horizontal (x) inertia forces, Coriolis force and centrifugal force induced by the moving distributed mass can be easily taken into the formulations by means of the last concept. To illustrate the application of the presented theory, the dynamic analysis of a pinned-pinned beam and that of a portal frame under the action of a moving uniformly distributed mass are performed by means of the finite element method and the Newmark integration method. Numerical results show that some pertinent factors, such as Coriolis force, centrifugal force, acceleration, velocity and total range of the moving distributed mass, have significant influences on the vertical (y) and horizontal (x) response of a structure.
Journal Article•10.1002/NME.1392•
Properties of time integration with first order filter damping

[...]

Steen Krenk1, Jan Riess Høgsberg1•
Technical University of Denmark1
28 Sep 2005-International Journal for Numerical Methods in Engineering
TL;DR: In this paper, an extra damping term in the form of a first order linear filter is added to the alpha weighted Newmark algorithm to remove undesirable low frequency damping and reduced order of accuracy.
Abstract: Introduction of algorithmic damping by increasing the parameter values in the Newmark algorithm leads to undesirable low-frequency damping and reduced order of accuracy It is demonstrated, how these effects can be removed by introducing an extra damping term in the form of a first order linear filter When the linear filter is discretized in time, the state variable associated with the filter can be eliminated, leading to a weighted average of the equations of motion at two consecutive times The filter procedure contains the known versions of alpha weighted Newmark methods as special cases, but gives a different and improved weighting of the excitation terms A complete analysis of the properties of the algorithm when used on linear systems is given, including the frequency response properties It is demonstrated that the effect of ‘overshoot’ is the consequence of a conservation relation that operates on a modified form of the mechanical energy of the system, and analytic results are presented for the magnitude of the effect Copyright © 2005 John Wiley & Sons, Ltd
On direct time integration in large deformation dynamic analysis

[...]

Mirza Muhammad, Irfan Baig, Klaus-Jürgen Bathe
1 Jan 2005
TL;DR: In this article, a composite Newmark method is proposed for nonlinear analysis problems, and the results obtained using the trapezoidal rule and the composite formula in a test problem are given.
Abstract: Direct time integration is used widely for the solution of large deformation problems in solid and structural mechanics. Direct integration schemes that are unconditionally stable for linear dynamic problems are also used for nonlinear problems. However, unconditional stability may be lost in the nonlinear regime. The Newmark method (trapezoidal rule) is used widely but may become unstable when large deformations and long time durations are considered. A composite scheme is proposed for such analysis cases, and the results obtained using the trapezoidal rule and the composite formula in a test problem are given. These results indicate the value of the composite scheme.
Journal Article•10.1103/PHYSREVE.72.046713•
Numerical method for interaction between multiparticle and complex structures.

[...]

Kensuke Yokoi1•
University of California, Los Angeles1
28 Oct 2005-Physical Review E
TL;DR: A numerical method that can treat the interaction between multiparticle and complex structures robustly and represented on a grid by using the level set method is proposed.
Abstract: We propose a numerical method for dealing with interactions between multiple particles and complex structures. In the method, the structures are represented on a grid by using the level set method. The interactions of particles and structures are calculated by a method based on the discrete element method. The method can treat the interaction between multiparticle and complex structures robustly.
Journal Article•10.1016/J.JSV.2004.02.003•
A transient response analysis in the state-space applying the average velocity concept

[...]

Byung Ok Kim, An Sung Lee
22 Mar 2005-Journal of Sound and Vibration
TL;DR: In this article, an implicit direct-time integration method for obtaining transient responses of general dynamic systems is described, based on the average velocity concept, which can be applied to an analysis of generalized dynamic systems expressed by state-space first-order differential equations.
Journal Article•10.1115/1.1934648•
Newmark’s Time Integration Method From the Discretization of Extended Functionals

[...]

Lorenzo Bardella1, Francesco Genna1•
University of Brescia1
01 Jul 2005-Journal of Applied Mechanics
TL;DR: This note illustrates how to obtain the full family of Newmark 's time integration algorithms within a rigorous variational framework, i.e., by discretizing suitably defined extended functionals, rather than by starting from a weak form (for instance, of the Galerkin type), as done in the past.
Abstract: In this note we illustrate how to obtain the full family of Newmark 's time integration algorithms within a rigorous variational framework, i.e., by discretizing suitably defined extended functionals, rather than by starting from a weak form (for instance, of the Galerkin type), as done in the past. The availability of functionals as a starting point is useful both as a tool to obtain new families of time integration methods, and as a theoretical basis for error estimates. To illustrate the first issue, here we provide some examples of how to obtain modified algorithms, in some cases significantly more accurate than the basic Newmark one despite having a comparable computational cost.
Journal Article•10.2507/IJSIMM04(1)•
Dynamic response simulation of planetary gears by the iterative spectral method

[...]

F. Chaari
15 Mar 2005-International Journal of Simulation Modelling
TL;DR: In this paper, a planetary gear is modeled and the equations of motion and the eigenfrequencies are recovered using the spectral iterative method and the computation of the dynamic response is made using the frequency domain.
Abstract: A planetary gear is modeled in this work. The equations of motion and the eigenfrequencies are recovered. The computation of the dynamic response is made using the spectral iterative method. The procedure is based on a modal approach with developments in the frequency domain. This technique has been successfully used and its convergence was quickly reached. Good agreement was obtained compared with the standard Newmark method. The dynamic response of the planetary gear is given directly in the frequency domain. The inverse Fourier transform gives the time response of the system.
Wind tunnel test and theoretical analysis on aeroelastic model of single-rod transmission tower

[...]

Wang Shi-cun
1 Jan 2005
TL;DR: In this article, an aeroelastic model of a single-rod transmission tower was tested in a wind tunnel to study its response to different wind velocity, under different circumstances with and without wires.
Abstract: As to the characteristic of large wind-induced response, an aeroelastic model of single-rod transmission tower was tested in a wind tunnel to study its response to different wind velocity. Under different circumstances with and without wires, the dynamic along-wind response and across-wind response in the turbulence flow and the aerodynamic force coefficients in the laminar flow were measured respectively. on the basis of that, the maximum acceleration, displacement, the proportion of across-wind response to (along-wind) response and the damping effect of wires were obtained, all of which can be used in structure (design.) Furthermore, the dynamic response was calculated with triangle series superposition method and Newmark method in time domain and with the power spectrum integral method in frequency domain respectively. The results were compared and the accuracy of the test was verified.
Effect of Internal Flow on Vortex-Induced Vibration of Submarine Free Spanning Pipelines

[...]

Lou Min1•
Ocean University of China1
1 Jan 2005
TL;DR: In this article, the effect of internal flow on the vortex-induced vibration of the free spans of a submarine free spanning pipeline was investigated and the Newmark method combined with simple iteration was used to solve the system of equations.
Abstract: At present, most researches on the vortex-induced vibration of submarine free spanning pipelines ignore the effect of internal flowing fluid; furthermore, there are no research reports considering the coupling effect of internal and external fluid with the free span. In this paper, combining Iwan's wake oscillator model with the differential equation derived for the dynamic response of submarine free spanning pipelines with inclusion of internal flow, the pipe-fluid coupling equations are developed to investigate the effect of internal flow on the vortex-induced vibration of the free spans. The finite element approximation is implemented to derive the matrix equations of equilibrium. The Newmark method combined with simple iteration is used to solve the system of equations. The results indicate that the internal fluid flow may cause the shift of resonance band to the lower frequency and a slight decrease in the peak value; the effect will be more pronounced with the increase of the span length and can be weakened in the presence of the axial tension.
Journal Article•10.1007/BF02440082•
Effect of damage on nonlinear dynamic properties of viscoelastic rectangular plates

[...]

郑玉芳1, 傅衣铭1•
Hunan University1
18 Mar 2005-Applied Mathematics and Mechanics-english Edition
TL;DR: In this paper, the nonlinear dunamic behaviors of viscoelastic rectangular plates including the damage effects under the action of a transverse periodic load were studied using the von Karman equations, Boltzmann superposition principle and continuum damage mechanics.
Abstract: The nonlinear dunamic behaviors of viscoelastic rectangular plates including the damage effects under the action of a transverse periodic load were studied. Using the von Karman equations, Boltzmann superposition principle and continuum damage mechanics, the nonlinear dynamic equations in terms of the mid-plane displacements for the viscoelastic thin plates with damage effect were derived. By adopting the finite difference method and Newmark method, these equations were solved. The results were compared with the available data. In the numerical calculations, the effects of the external loading parameters and geometric dimensions of the plate on the nonlinear dynamic responses of the plate were discussed. Research results show that the nonlinear dynamic response of the structure will change remarkably when the damage effect is considered.
Journal Article•10.1142/S0219455405001477•
Errors in numerical solution of equation of motion of lightly damped sdof system near resonance

[...]

Aleksandar Pavic1, Stana Živanović1, Paul Reynolds1•
University of Sheffield1
01 Mar 2005-International Journal of Structural Stability and Dynamics
TL;DR: In this paper, the authors investigated the error which occurs when numerically integrating the equation of motion of a single degree of freedom system excited by a harmonic force near resonance, and provided recommendations as to the time steps required to obtain solutions with a pre-defined level of accuracy.
Abstract: This study investigates the error which occurs when numerically integrating the equation of motion of a single degree of freedom system excited by a harmonic force near resonance. The Constant Average Acceleration method was considered in particular as it features in many finite element software packages. It was found that a considerable error in the calculated responses occurs in systems with low damping due to the well known phenomenon of period elongation. However, the error is reduced for systems with higher damping and/or when smaller time step is used. With regard to this, recommendations are given as to the time steps required to obtain solutions with a pre-defined level of accuracy.
Effect of Internal Flow on Vortex-Induced Vibration of Submarine Free Spanning Pipelines

[...]

娄敏, 丁坚, 郭海燕, 董晓林
1 Jan 2005
TL;DR: In this paper, the effect of internal flow on the vortex-induced vibration of the free spans of a submarine free spanning pipeline was investigated and the Newmark method combined with simple iteration was used to solve the system of equations.
Abstract: At present, most researches on the vortex-induced vibration of submarine free spanning pipelines ignore the effect of internal flowing fluid; furthermore, there are no research reports considering the coupling effect of internal and external fluid with the free span. In this paper, combining Iwan's wake oscillator model with the differential equation derived for the dynamic response of submarine free spanning pipelines with inclusion of internal flow, the pipe-fluid coupling equations are developed to investigate the effect of internal flow on the vortex-induced vibration of the free spans. The finite element approximation is implemented to derive the matrix equations of equilibrium. The Newmark method combined with simple iteration is used to solve the system of equations. The results indicate that the internal fluid flow may cause the shift of resonance band to the lower frequency and a slight decrease in the peak value; the effect will be more pronounced with the increase of the span length and can be weakened in the presence of the axial tension.
Journal Article•10.1007/S10409-005-0058-2•
Analysis of nonlinear vibration for symmetric angle-ply laminated viscoelastic plates with damage

[...]

Yufang Zheng1, Yiming Fu1•
Hunan University1
02 Sep 2005-Acta Mechanica Sinica
TL;DR: In this paper, the behavior of nonlinear vibration for symmetric angle-ply laminated plates including the material viscoelasticity and damage evolution is investigated by employing the von Karman's nonlinear theory, strain energy equivalence principle and Boltzmann superposition principle.
Abstract: The behavior of nonlinear vibration for symmetric angle-ply laminated plates including the material viscoelasticity and damage evolution is investigated. By employing the von Karman's nonlinear theory, strain energy equivalence principle and Boltzmann superposition principle, a set of governing equations of nonlinear integro-differential type are derived. By applying the finite difference method, Newmark method and iterative procedure, the governing equations are solved. The effects of loading amplitudes, exciting frequencies and different ply orientations on the critical time to failure initiation and nonlinear vibration amplitudes of the structures are discussed. Numerical results are presented for the different parameters and compared with the available data.
Journal Article•10.1533/IJCR.2005.0357•
Nonlinear impact behaviour of laminated composite shells in hygrothermal environments

[...]

N. V. Swamy Naidu, P.K. Sinha
01 Apr 2005-International Journal of Crashworthiness
TL;DR: In this paper, the nonlinear transient response of laminated composite shell panels subjected to low velocity impact in hygrothermal environments is investigated using finite element method, where a modified Hertzian contact law is incorporated into the finite element program to evaluate the impact force.
Abstract: The nonlinear transient response of laminated composite shell panels subjected to low velocity impact in hygrothermal environments is investigated using finite element method. The present formulation considers doubly curved thick shells and includes large deformations with Green- Lagrange strains. The analysis is carried out using quadratic eight—noded isoparametric element. A modified Hertzian contact law is incorporated into the finite element program to evaluate the impact force. The nonlinear equation is solved using the Newmark average acceleration method in conjunction with an incremental modified Newton-Raphson scheme. The validity of the present analysis is demonstrated by comparing the present results with the solutions available in the literature. A parametric study is carried out to investigate the effects of the curvature and side to thickness ratios of simply supported composite cylindrical and spherical shell panels.
Effect of damage on nonlinear dynamic properties of viscoelastic rectangular plates

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Zheng Yu
1 Jan 2005
TL;DR: In this article, the nonlinear dynamic behaviors of viscoelastic rectangular plates including the damage effects under the action of a transverse periodic load were studied using the von Karman equations, Boltzmann superposition principle and continuum damage mechanics.
Abstract: The nonlinear dynamic behaviors of viscoelastic rectangular plates including the damage effects under the action of a transverse periodic load were studied Using the von Karman equations, Boltzmann superposition principle and continuum damage mechanics, the nonlinear dynamic equations in terms of the mid_plane displacements for the viscoelastic thin plates with damage effect were derived By adopting the finite difference method and Newmark method, these equations were solved The results were compared with the available data In the numerical calculations, the effects of the external loading parameters and geometric dimensions of the plate on the nonlinear dynamic responses of the plate were discussed Research results show that the nonlinear dynamic response of the structure will change remarkably when the damage effect is considered
Journal Article•10.12989/SEM.2005.20.1.111•
Dynamic interaction analysis of vehicle-bridge system using transfer matrix method

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Tianyu Xiang, Renda Zhao
10 May 2005-Structural Engineering and Mechanics
TL;DR: In this article, the dynamic interaction of vehicle-bridge is studied by using transfer matrix method in which the vehicle model is simplified as a spring-damping-mass system and the partial differential equation of structure vibration is transformed into a differential equation irrelevant to time.
Abstract: The dynamic interaction of vehicle-bridge is studied by using transfer matrix method in this paper. The vehicle model is simplified as a spring-damping-mass system. By adopting the idea of Newmark-b method, the partial differential equation of structure vibration is transformed into a differential equation irrelevant to time. Then, this differential equation is solved by transfer matrix method. The prospective application of this method in real engineering is finally demonstrated by several examples.

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