Abstract

In a recent paper of the authors, a novel nodal-based floating frame of reference formulation (FFRF) for solid finite elements has been proposed. The nodal-based approach bypasses the unhandy inertia shape integrals ab initio, i.e. they neither arise in the derivation nor in the final equations of motion, leading to a surprisingly simple derivation and computer implementation without a lumped mass approximation, which is conventionally employed within commercial multibody codes. However, the nodal-based FFRF has so far been presented without modal reduction, which is usually required for efficient simulations. Hence, the aim of this follow-up paper is to bring the nodal-based FFRF into a suitable form, which allows the incorporation of modal reduction techniques to reduce the overall system size down to the number of modes included in the reduction basis, which further reduces the computational complexity significantly. Moreover, this exhibits a way to calculate the so-called FFRF invariants, which are constant “ingredients” required to set up the FFRF mass matrix and quadratic velocity vector, without integrals and without a lumped mass approximation.

Highlights

  • The floating frame of reference formulation (FFRF) is one of the most widely used methods to analyse flexible multibody systems and is implemented in most commercial flexible multibody dynamics codes

  • The formulation is applicable to flexible multibody systems subjected to large rigid body translations and rotations but small strains and flexible deformations with respect to the floating frame, such as vehicles, aircraft, robots, and machines

  • The aim of this follow-up paper is to bring the nodal-based FFRF into a suitable form, which allows the incorporation of modal reduction techniques to reduce the overall system size down to the number of modes included in the reduction basis and to render the aforementioned matrix operations unnecessary, which further reduces the computational complexity significantly

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Summary

Introduction

The floating frame of reference formulation (FFRF) is one of the most widely used methods to analyse flexible multibody systems and is implemented in most commercial flexible multibody dynamics codes. In recent papers of the authors [20, 21], a novel nodal-based FFRF for solid FEs has been proposed This nodal-based approach bypasses the inertia shape integrals ab initio, i.e. the integrals arise neither in the derivation nor in the final expression of the equations of motion (EOMs), leading to a surprisingly simple derivation and computer implementation without a lumped mass approximation. The aim of this follow-up paper is to bring the nodal-based FFRF into a suitable form, which allows the incorporation of modal reduction techniques to reduce the overall system size down to the number of modes included in the reduction basis and to render the aforementioned matrix operations unnecessary, which further reduces the computational complexity significantly This will reveal a possibility to calculate the FFRF invariants without a lumped mass approximation and, without inertia shape integrals.

Non-reduced equations of motion of the nodal-based FFRF
A suitable form of the nodal-based FFRF to enable a proper modal reduction
Nodal-based FFRF invariants without a lumped mass approximation
Nodal-based modally reduced FFRF mass matrix and quadratic velocity vector
Nodal-based modally reduced FFRF applied generalized forces
From 3D to 2D spaces
Modally reduced nodal-based FFRF in 2D space
Slider–crank mechanism
A short note on the consequences of a lumped mass approach
Conclusions
Full Text
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