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2013 | OriginalPaper | Chapter

6. Finite Elements

Author : André Preumont

Published in: Twelve Lectures on Structural Dynamics

Publisher: Springer Netherlands

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Abstract

This is the second chapter devoted to the approximate analysis of continuous systems. In the finite element method, the shape functions are defined within the element, once and for all, with the generalized coordinates being the nodal displacements and rotations. The method is also based on Hamilton’s principle; the element stiffness and mass matrices of the approximate discrete system are obtained by expressing the strain energy and the kinetic energy in terms of the generalized coordinates. This chapter considers the finite element formulation of a plane truss (made of bar elements) and of planar structures made of beams, including the geometric stiffness. The convergence of the finite element method is briefly addressed. The chapter concludes with a discussion of the methods for model reduction: Guyan method and Craig-Bampton method. A set of problems is proposed at the end of the chapter.

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Footnotes
1
Observe that these shape functions are such that any rigid body motion such that \(\theta _1=\theta _2\) and \(v_2=v_1+\theta _1 l\) will lead to a linear distribution of the transverse displacements: \(v(x)=v_1+\theta _1 x\).
 
2
In Sect. 4.​3 devoted to the analysis of continuous beams, the reduced eigenvalue was defined as
$$\begin{aligned} \mu ^4=\frac{\varrho AL^4}{EI}\omega ^2 \end{aligned}$$
where \(L\) is the length of the beam; in this case, \(L=2l\).
 
3
This model leads to a buckling load of \(P_{cr}=20EI/l^2\), instead of the analytical value of \(P_{cr}=2\pi ^2EI/l^2\) obtained in Sect. 5.​6.​1 when using the analytical buckling shape as shape function.
 
4
The finite element method provides the best solution in the family of possible shape functions; in this case, the third order polynomials contain the analytical solution.
 
5
It does not matter which variable of \(u_2\) and \(\theta _2\) is kept in the final model; the choice of \(u_2\) as slave coordinate was made when the first row of the stiffness matrix was adopted.
 
Metadata
Title
Finite Elements
Author
André Preumont
Copyright Year
2013
Publisher
Springer Netherlands
DOI
https://doi.org/10.1007/978-94-007-6383-8_6

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