OptiStruct is a proven, modern structural solver with comprehensive, accurate and scalable solutions for linear and nonlinear
analyses across statics and dynamics, vibrations, acoustics, fatigue, heat transfer, and multiphysics disciplines.
The OptiStruct Example Guide is a collection of solved examples for various solution sequences and optimization types and provides
you with examples of the real-world applications and capabilities of OptiStruct.
This section presents nonlinear small displacement analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents nonlinear large displacement analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents nonlinear transient analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents normal modes analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents complex eigenvalue analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents thermal and heat transfer analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents analysis technique examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents shape optimization example problems, solved using OptiStruct. Each example uses a problem description, execution procedures and results to demonstrate how OptiStruct is used in shape optimization.
The examples in this section demonstrate how topography optimization generates both bead reinforcements in stamped
plate structures and rib reinforcements for solid structures.
A tube made of two sheet metal pieces is intended to carry a load in both bending and torsion. The cross-section of
the tube may be of any shape, but due to manufacturing requirements, it must remain constant through the entire length.
A rectangular thin-walled box is to be used to store fluid. The outward bulging of the sides of the container (due
to the pressure of the contents) is to be minimized. Additionally, the maximum outward displacement of the side panels
must be below a given value.
This example involves a rectangular, thin-walled container used for storing fluid. The objective is to minimize the
outward bulging of the sides of the container caused by the pressure of its contents. Additionally, the maximum outward
displacement of the side panels must be below a given value.
Finding a good reinforcement pattern for a single modal frequency is difficult when dealing with beaded plates since
adding stiffness in one direction often reduces stiffness in another direction.
Topography optimization has applications beyond creating beads in shell surfaces. Since the basic topography approach
can be applied to any model containing large fields of shape variables, it lends itself to solid model applications,
as well.
Pattern grouping lends itself very well to applications where manufacturing conditions must be met. In this example,
topography optimization is used to form a design concept out of a solid block. Manufacturing the design concept using
a casting method is preferable.
The examples in this section demonstrate how the Equivalent Static Load Method (ESLM) can be used for the optimization
of flexible bodies in multibody systems.
This section presents multiphysic examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents response spectrum examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents nonlinear explicit analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
This section presents piezoelectric analysis examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used.
The OptiStruct Example Guide is a collection of solved examples for various solution sequences and optimization types and provides
you with examples of the real-world applications and capabilities of OptiStruct.
The examples in this section demonstrate how topography optimization generates both bead reinforcements in stamped
plate structures and rib reinforcements for solid structures.
A tube made of two sheet metal pieces is intended to carry a load in both bending and torsion. The cross-section of
the tube may be of any shape, but due to manufacturing requirements, it must remain constant through the entire length.
OS-E: 3000 Cross-section Optimization of a Spot Welded Tube
A tube made of two sheet metal pieces is intended to carry a load in both bending and
torsion. The cross-section of the tube may be of any shape, but due to manufacturing
requirements, it must remain constant through the entire length.
Model Files
Before you begin, copy the file(s) used in this example to
your working directory.
Conventional shape optimization can be used to optimize the cross-section, but
setting up the variables is time consuming. With topography optimization and pattern
grouping, cross-section shape optimization can be performed in a fraction of the set
up time. All optimization set up is done using the Optimization panel and its subpanels in HyperMesh.
The loads and constraints are applied to the flanges at the ends of the tube, and are
shown in Figure 1. Spot welds connect the two pieces of the tube along the flanges at regular
intervals.
The initial cross-section of the tube is arbitrarily chosen to be roughly circular.
Two similar topography variables are defined to allow the shape of the tube to
change. The two variables assign the blue and green pieces to be in the design
domain while the flanges remain in their original shape. The topography variables
are in the Bulk Data section using the DTPG card as.
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
DTPG
1
PSHELL
1
+
2.5
85.0
NO
5.0
NORM
NONE
+
PATRN
1
0.0
0.0
0.0
1.0
0.0
0.0
The draw height of 5.0, combined with the upper and lower bounds of 2.0 and -2.0,
allow a bead height of 10.0 model units in both directions (inward and outward) and
a bead growth direction normal to the surface of the tube. A linear type pattern
grouping is applied for this problem. This means that the beads formed during the
topology optimization will be constant along a line parallel to the direction
defined -- the central axis (X-axis) of the tube, in this case. By setting this
pattern grouping option, the cross-section of the tube will be allowed to change,
but will remain constant through the length of the tube.
The objective was set to minimize the weighted compliance of both load cases. In this
case, both load cases were weighted equally. The mass of the tube was constrained to
be below the initial value. OptiStruct generated the
following solution for the model (Figure 2).
The solution is not completely smooth, but the basic shape of the tube is clear. The
lower half of the tube has been lowered to increase the bending stiffness of the
section while the upper half of the tube runs directly from one flange to the other
to support the shear force generated by the twist load (Figure 3).
Results
To verify the OptiStruct solution, a smooth model of the
tube is built based upon the results. This model is shown in Figure 4 and Figure 5. Static analysis shows the optimized cross-section after smoothing to have a 35%
lower peak deflection for torsion and an 18% lower peak deflection for bending.
Additionally, the mass of the part was reduced by 2.2%.