Choice of Elements

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Simulation Keep it SIMPLE & SMART
Shakeel Mirza – Technical Consultant-Autodesk
Speaker
Michael Smell-Technical Consultant-Autodesk
Co-Speaker
MA7404-P
Learning Objectives
At the end of this class, you will be able to:

Simplify complex physical problems

Reduce overall simulation setup and runtime to half or even more

Handle larger models

Interpret results easily
About the Speaker
As a mechanical engineer with a master's degree in mechanical modeling and simulation,
since starting his career, Shakeel Mirza has been involved and focused on mechanical
simulations. He has worked in domains such as: automobile crash simulation, plastic parts
structural analysis, crack modeling in pressure vessels, optimization for onboard components
for aircraft, steel and concrete building, bridge design and analysis, and customization of
analysis software for specific applications for non-experts. He has worked with different CAE
tools under different CAD environments for a vast variety of industrial applications as a CAE
application engineer, and as a consultant. Recently, he has been involved in the
implementation of Autodesk® Simulation solutions at strategic accounts worldwide.
shakeel.mirza@autodesk.com
Simulation Keep it SIMPLE & SMART
Geometric Simplifications:
Suppress Unnecessary Parts or Features:
From an analysis perspective, unnecessary features or even parts can be suppressed from a
model. An unnecessary feature can be a small radius fillet or a hole whose presence will not
have a significant impact on the stresses in critical zones. In such cases it’s helpful to suppress
those features as this will allow work on a much lighter model.
Typical mechanical assemblies consist of parts, fasteners and various constraining parts.
Although all parts might not be critical from a design perspective, they still play an important role
to join parts together or impose particular motion constraints.
Such parts can be suppressed for FEA as long as their role can be modeled by simple
representation. For example in case of a bolt, holding together two parts firmly, the bolt can be
suppressed and the two parts can be modeled as joined together using contacts or other
simplified models. Same holds true for welds, rivets and pins.
However if the parts are creating a special state in the model, for example a bolt with significant
pretension, it needs to be modeled with more details.
Exploit Symmetry:
When creating a model for finite element analysis, natural lines of symmetry and antisymmetry
can allow you to analyze a structure or system by modeling only a portion of it. This technique
can reduce the size of the model (the total number of nodes and elements), which can reduce
the analysis run time as well as the demands on computer resources.
Required Conditions to Exploit Symmetry in a Model
To take advantage of the symmetrical modeling technique, the following conditions for
symmetry (or antisymmetry) must exist:
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
the geometry, material properties and boundary conditions are symmetric
the loading is symmetric or antisymmetric.
It’s required to build a model of the symmetrical portion (half, quarter, eighth, etc.) and apply the
appropriate boundary conditions. This consists of isolating the symmetric portion from the
complete model.
Advantages of a symmetrical/antisymmetrical model include the following:
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Faster model preprocessing, meshing and post processing
A finer mesh of the symmetrical model for greater accuracy can be generated
Far less computational resources required (Disk space, memory, processor speed)
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Simulation Keep it SIMPLE & SMART
Planar or Mirror Symmetry
Planar or Mirror Symmetry means a model is identical on either side of a dividing line or plane
(see Figures 1-3). Along the line or plane of symmetry, boundary conditions must be applied to
represent the symmetrical part as follows:

Out-of-plane displacement = 0

The two in-plane rotations = 0
Figure 1: Model with a Line of Symmetry
Figure 2: Model with a Plane of Symmetry
Figure 3: Example of Symmetry for Plate Elements
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Simulation Keep it SIMPLE & SMART
Antisymmetry
Antisymmetry means the loading of a model is oppositely balanced on either side of a dividing
line or plane (see Figures 4-5). Boundary conditions must be applied along the line of symmetry
as follows:
1. Out-of-plane rotation = 0
2. The two in-plane displacements = 0
Figure 4: Antisymmetrical Model
.
Figure 5: Example of Antisymmetry for Plate Elements
Figure below shows an antisymmetrical boundary condition in Autodesk Simulation software.
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Simulation Keep it SIMPLE & SMART
Cyclic symmetry
Cyclic symmetry occurs when the geometry, loads, constraints and results of a partial model
can be copied around an axis to give the complete model. A typical example is a fan blade or
turbine. If the loads on the blades and geometry repeat, only one blade needs to be modeled
instead of the entire hub of X blades. See figure below. The result is a smaller analysis which
takes less time to analyze.
Figure above shows a Cyclic Symmetry Example (the highlighted section, including the load,
can be copied 7 times about the axis O to create the full model)
In particular, cyclic symmetry forces the radial, tangential, and axial displacements at the nodes
on one face (A in Figure) to match the same nodes on the opposite face (B in Figure).
When Not to Use Symmetric Models:
The evident case were symmetric model are to be avoided is where the model contains a
feature that disrupts the symmetry and can create significant unsymmetrical behavior. A hole in
one of the fan blades can be considered as a simple example.
Apart from that, under certain circumstances, it’s not possible to exploit symmetry even though
the model, material, loads and supports might be symmetric.
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Simulation Keep it SIMPLE & SMART
Basically whenever the expected results are non-symmetrical, symmetric models must not be
considered.
For example in case of a modal analysis of a symmetric model, one can expect very well to see
unsymmetrical modes of vibration. These modes will not be captured if a symmetric model is
being used.
Same holds true for buckling analysis. An axisymmetric analysis of a hollow pipe will give the
critical load of buckling of the first axisymmetric mode; while in reality the pipe will buckle at a
much lower load in an unsymmetrical mode.
Choice of Elements
Another very powerful time saving technique is the choice of best suited element for an
analysis. This is based upon the primary and secondary variable that is being sought as output
from the analysis.
1. 3D-Solid Elements
Three dimensional solid elements are the easiest to use and simply discretize a three
dimensional geometry (solid part) into smaller finite elements. They don’t require any
preparation of model for geometry. They are best suited for massive parts (molded, casted
,forged parts)
To capture bending in thin models with solid elements, three elements should be created
through the thickness. If this cannot be done for the model and is needed, the model may need
to be evaluated using plate elements.
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Simulation Keep it SIMPLE & SMART
2. 2D Elements:
Certain specific cases can be represented in 2D. 2D elements can be used if the expected
behavior is symmetric in one of the 3D dimensions.
Three main types of 2D elements are:
1. Plane Stress
2. Plane Strain
3. Axisymmetric
The first three types are not only geometrically 2D (that is without thickness explicitly modeled)
but should strictly lie in a 2D plane. Plate and Shell elements can be drawn in 2D but can
assume any shape in 3D space.
2D elements are three- or four-node elements that must be formulated in the YZ plane. They
are used to model and analyze objects such as bearings or seals, or structures such as dams.
These elements are formulated in the YZ plane and have only two degrees-of-freedom defined:
the Y translation and the Z translation. Temperature-dependent orthotropic material properties
can be defined and incompatible displacement modes can be included.
When to Use 2D Elements:
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
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To model a cross section of a part.
Plane stress geometry type: No stress in the X direction (through the thickness). Strain
in the X direction is allowable (for example, thin plate under an axial load).
Plane strain geometry type: No strain in the X direction (through the thickness). Stress in
the X direction is allowable (for example, large dam).
Axisymmetric geometry type: Model is axisymmetric about the Z axis and exists only in
the positive Y quadrant of the YZ plane.
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Simulation Keep it SIMPLE & SMART
3. Shell Elements:
These elements are used to model thin plate/shell type structures in 3D space. As a general
rule they represent the mid-surface of a thin solid without any thickness modeled as part of the
geometry but defined as an element attribute to model the correct stiffness. The huge
advantage of shells is that the user doesn’t need to worry about the recommended “three
elements in the thickness” for thin solids.
Typical Shell Elements
Each shell element node has 5 degrees of freedom (DOF) - three translations and two rotations.
The translational DOF are in the global Cartesian coordinate system. The rotations are about
two orthogonal axes on the shell surface defined at each node. The rotational boundary
condition restraints and applied moments also refer to this nodal rotational system.
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Simulation Keep it SIMPLE & SMART
4. 1D or Line Elements:
These types of elements are used to model thin slender members like beams, trusses, cables
etc. They essentially consist of a line with attributes such as cross-section properties. They are
used to represent structures of length much greater than the width or depth (approximately 8-10
times).
Beam and truss elements are the most common types from 1D element family among others.
Beam elements are two-node members which allow arbitrary orientation in the 3D (threedimensional) X, Y, Z space. An additional node (K-node) is required to define the element
orientation. The beam transmits moments, torque and forces and is a general six (6) degree of
freedom (DOF) element (three global translation and rotational components at each end of the
member).
Truss Elements on the other hand are similar in construction as beams but without the ability to
transmit moments, they can be considered as beams that are pinned together hence the name
truss. Trusses, by definition, cannot have rotational DOFs.
Truss elements are two-node members which allow arbitrary orientation in the XYZ coordinate
system. The truss transmits axial force only and, in general, is a three degree-of-freedom (DOF)
element. They are used to model structures such as towers, bridges, and buildings.
The three-dimensional (3D) truss element is assumed to have a constant cross-sectional area
which is defined as an element attribute
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