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CAD is traditionally seen as the carrier of information in design. However,
creating a finite element analysis model of a design invariably requires
simplification. Therefore, the analysis model is often rebuilt from
scratch, relying upon the judgment of skilled analysts, much of the work
in creating the geometry being duplicated. As well as removing details
from the design geometry, plate, shell and beam element types are also
often used where they can give more accurate and cost effective results.
Procedures have been developed for the automatic dimensional reduction
of a 2D geometric model to an equivalent 1D beam analysis model. This was
achieved using the medial axis transform, an alternative skeleton-like representation of the
geometric model having properties relevant to model simplification. Mixed
dimensional models are created implicitly with the required coupling automatically
applied. Click here for more information on automatic dimensional reduction.
Operations have also been defined and implemented for the expansion of
these operations to the dimensional reduction of 3D solid models to equivalent
solid/shell/beam analysis models. These operations are interactive,
with appropriate physical properties such as shell thickness, beam section
moment of areas and torsion constants calculated automatically.
The automatic dimensional reduction of thin walled solids to equivalent
shell models has been implemented using a geometric measure similar to
an aspect ratio, but extended for solid to shell dimensional reduction.
This process uses the operations described earlier directly, with shell
thicknesses being calculated automatically.
The first stage is to subdivide the 2D model into subregions which are
suitable for representation by 1D beam elements, and those which are not
to either by 2D elements, or by an equivalent 0D point mass.
A threshold value of aspect ratio can then be introduced, below which a
region is not suitable for representation as 1D beam elements and must
be represented either by the 2D region or an equivalent 0D point mass.
All other regions can then be represented by 1D beams.
For the case of mixed 1D/0D abstracted models, the 1D beams can either
be connected together with rigid links, or extrapolated to meet at their
closest point inside the neighbouring 0D region.
The diagram below shows a 2D axisymmetric section of part of a turbine casing. They were used here to validate the dimensionally reduced beam models created. A natural frequency analysis of both the 2D sections and the abstracted beam models was carried out. The results for the first three modes are presented below. Three analyses were carried out, namely for a full 2D mesh, a 1D model with rigid link coupling and an extrapolated 1D beam model. Also shown is the extrapolated beam model (top left), the beams together with 2D regions represented as point masses in the analysis model (centre left) and the beam model coupled with rigid links (bottom left).



