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.
A uniform, homogeneous plate which is symmetric about horizontal axes in both geometry and loading, to find the maximum
axial stress in the plate with a hole.
Snap-fit is a combination of two components namely mating and base part which form a mechanical attachment between them
by means of locators, locks and enhancements. Nonlinear Static Analysis with large displacement theory is used to solve
this example.
Contact smoothing is useful to increase accuracy of the contact solution. An enforced displacement to push two concentric
rings toward each other to engage the contact is used. The usage of NLOUT entry allows you to study the progression of SPC force over successive increments.
Demonstrate a revolute joint using JOINTG and MOTNJG. The JOINTG entry can be used for defining a variety of joints, including revolute, ball, universal, cardan, and so on. Motion on
these joints can be applied using the MOTNJG entry.
Demonstrates self-contact which is used in this nonlinear large displacement implicit analysis involving hyperelastic
material and contacts using OptiStruct.
This section presents optimized topology examples generated using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used as a design concept tool.
This section presents size (parameter) optimization examples solved using OptiStruct. Each example uses a problem description, execution procedures, and results to demonstrate how OptiStruct is used in size optimization.
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.
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.
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.
OS-E: 0125 Diagnose Non-converged Solution using NLMON
Modeled using solid and shell elements and when the solution is not converged, run
diagnostics modeling errors using NLMON.
Model Description
The cantilever beam model is shown in Figure 1, and both the elements joined by merging the common nodes. This
example simulation is with nonlinear static solution with large displacement.
FE Model
Element Types
CHEXA
CQUAD
MAT1
Young’s Modulus
2.1E5 MPA
Poisson Ratio
0.3
Density
7.8E
Results
Note: NLMON toolkit is for nonlinear convergence monitoring and debugging (load
NLMON_NL.h3d file). Import the TCL script from HyperView to launch NLMON utility tool from this location in the
HyperWorks installation:
<Altair_Home>\hwsolvers\scripts\ os_out_file_parser.tcl and load
the .out file in this utility to sync it with HyperView. NLMON works with large and small displacement
problems.
In the .out file, notice the max displacement
increment and correction is at node 13 (Figure 2). Load the NLMON_nl.h3d file and the
.out file using NLMON utility tool to sync. Click on the maximum
displacement increment or maximum displacement correction on the NLMON utility (Figure 4) and notice that elements (shell elements rotations) are
not clamped correctly (animate for better visualization) in HyperView page, as shown in Figure 3
.
Tip: To improve convergence, use TIE or
FREEZE contact to connect shell and solid elements.