1. How to compute invariant manifolds and their reduced dynamics in high-dimensional finite element models
- Author
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George Haller and Shobhit Jain
- Subjects
FOS: Computer and information sciences ,Lyapunov function ,Dynamical systems theory ,Discretization ,Computer science ,Finite elements ,Aerospace Engineering ,Ocean Engineering ,Dynamical Systems (math.DS) ,Degrees of freedom (mechanics) ,Normal forms ,Computational Engineering, Finance, and Science (cs.CE) ,symbols.namesake ,Spectral submanifolds ,Reduced-order modeling ,FOS: Mathematics ,Applied mathematics ,Mathematics - Dynamical Systems ,Electrical and Electronic Engineering ,Invariant (mathematics) ,Computer Science - Computational Engineering, Finance, and Science ,Partial differential equation ,Applied Mathematics ,Mechanical Engineering ,Finite element method ,Nonlinear system ,Invariant manifolds ,Control and Systems Engineering ,symbols ,Lyapunov subcenter manifolds ,Center manifolds - Abstract
Invariant manifolds are important constructs for the quantitative and qualitative understanding of nonlinear phenomena in dynamical systems. In nonlinear damped mechanical systems, for instance, spectral submanifolds have emerged as useful tools for the computation of forced response curves, backbone curves, detached resonance curves (isolas) via exact reduced-order models. For conservative nonlinear mechanical systems, Lyapunov subcenter manifolds and their reduced dynamics provide a way to identify nonlinear amplitude-frequency relationships in the form of conservative backbone curves. Despite these powerful predictions offered by invariant manifolds, their use has largely been limited to low-dimensional academic examples. This is because several challenges render their computation unfeasible for realistic engineering structures described by finite element models. In this work, we address these computational challenges and develop methods for computing invariant manifolds and their reduced dynamics in very high-dimensional nonlinear systems arising from spatial discretization of the governing partial differential equations. We illustrate our computational algorithms on finite element models of mechanical structures that range from a simple beam containing tens of degrees of freedom to an aircraft wing containing more than a hundred-thousand degrees of freedom., Nonlinear Dynamics, 107 (2), ISSN:0924-090X, ISSN:1573-269X
- Published
- 2021
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