Computer-Aided Design 42 (2010) 808–816
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Computer-Aided Design
journal homepage: www.elsevier.com/locate/cad
Algebraic reduction of beams for CAD-integrated analysis
Kavous Jorabchi, Joshua Danczyk, Krishnan Suresh
∗
2050 Mechanical Engineering, 1513 University Ave, Madison, WI 53706, University of Wisconsin, Madison, United States
article info
Article history:
Received 16 October 2007
Accepted 6 May 2010
Keywords:
Beams
Finite element analysis
CAD-integrated analysis
Dimensional reduction
abstract
Beams are high aspect ratio structural members that are used extensively in civil, automotive, aerospace,
and MEMS applications. In all such applications, one must typically analyze and optimize the beams
through computer simulations. Standard 3D finite element analysis (FEA) of beams can be used in such
simulations; it is however prone to errors, and is computationally expensive for thin structures. Therefore,
a common strategy is to carry out a dimensionally reduced 1D beam analysis. Unfortunately, 1D beam
analysis is hard to automate and integrate with 3D CAD.
In this paper, we propose an alternate ‘‘algebraic reduction’’ method that combines the generality of
3D FEA, and the computational efficiency of 1D beam analysis. This is achieved via a dual-representation
framework where the geometry of the beam is captured via a 3D finite element mesh, while the physics
is captured via a 1D beam model. The proposed method is formally established, and supported through
numerical experiments.
© 2010 Elsevier Ltd. All rights reserved.
1. Introduction
Beams
1
are high aspect ratio structural members. Due to
their high strength-to-weight ratio they are used extensively, for
example, in civil structures, automotive body panels, aerospace
structures, and MEMS applications. Fig. 1, for example, shows
a high aspect ratio micro-cantilever beam used as an MEMS
vibration sensor [1].
In theory, it is possible to analyze beams via standard 3D finite
element analysis [2]. However, the recommended strategy is 1D
beam analysis [3] for reasons discussed below (other less-common
methods are also reviewed later in this section).
Standard 3D finite element analysis (FEA) (see Fig. 2) has
reached a high degree of reliability over the past few decades,
making it the de facto analysis method today.
However, high aspect ratio beams pose unique challenges to
3D FEA. Specifically, consider the beam problem in Fig. 3(a). If one
uses a coarse finite element mesh (element size ≫ thickness) as
in Fig. 3(b), the presence of poor quality elements leads to Poisson
and shear locking [4].
On the other hand, if a high quality mesh (element size ∼
thickness) is used, the computational cost grows rapidly with the
aspect ratio as illustrated in Fig. 4 (aspect ratio is the overall length
divided by the thickness of the hollow beam).
∗
Corresponding author. Tel.: +1 608 262 3594; fax: +1 608 265 2316.
E-mail address: suresh@engr.wisc.edu (K. Suresh).
1
In this paper the word ‘‘beam’’ is used in two contexts: ‘‘beam’’ without any
prefix implies the actual 3D geometric model, whereas ‘‘1D beam’’ implies 1D (line)
idealization of the 3D geometry.
Thus, despite the generality and ease of 3D FEA, it is rarely used
today to analyze high aspect ratio structures.
Indeed, the recommended strategy for thin beam-like geome-
tries is 1D beam analysis [5]. This method entails explicitly com-
puting the 1D beam axis and extracting the cross-sectional prop-
erties (see Fig. 5); 1D beam analysis does not suffer from locking
and ill-conditioning problems, and is highly efficient.
However, 1D beam analysis poses numerous automation chal-
lenges. Specifically, as the beam becomes increasingly complex,
computing the 1D beam geometry from a 3D CAD model can be
cumbersome [6,7]. Further, coupling the 1D geometry to 3D struc-
tural elements is non-trivial (see Fig. 5). Finally, post-processing
and visualizing the 1D analysis results within the 3D environment
defeats the very purpose of 3D modeling.
Besides 3D FEA and 1D analysis, other methods have been
proposed for analyzing thin structures [8]. A popular method
is based on the concept of solid-shell elements that use an
anisotropic space for the finite element basis functions, i.e.,
relatively low order shape functions are used across the thickness
to overcome ill-conditioning, etc. However, solid-shell methods
entail a priori orientation of the finite element mesh [9], which can
pose difficulties for standard finite element mesh generators.
Reduced integration techniques have also been proposed by
several researchers to suppress the deficiencies of standard
FEA [10,11]; however, under-integration causes generation of
hourglass modes and needs stabilization. Yet another technique
is to use hybrid or mixed variational principles for stresses
and displacements [12]. Hybrid elements can be computationally
expensive since construction of the element stiffness entails
inverting a sizeable matrix [12].
0010-4485/$ – see front matter © 2010 Elsevier Ltd. All rights reserved.
doi:10.1016/j.cad.2010.05.001