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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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.
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
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.