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.
The PCOMPLS entry can be used to define continuum shell composites using solid elements. Currently first order CHEXA and CPENTA solid elements are supported.
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: 0160 Nonlinear Static Analysis of Snap Fit Assembly Using Continuous Sliding
Demonstrates the effect of continuous sliding in Nonlinear Static (large displacement)
Analysis.
Continuous sliding allows for the incorporation of continuous (large) relative sliding
between the master and slave. Contact is updated for every iteration. Continuous sliding
contact is expected to produce more accurate results and in some cases, better convergence
robustness, especially when very large sliding and/or distortion are present.
Figure 1. FE Model
Model Description
The Finite element model shown in Figure 1, is constrained with symmetric boundary conditions and
applied prescribed displacement in the X-axis.
FE Model
Elements Types
CTETRA
RBE2
The linear material properties are:
MAT1
Young’s Modulus
5E3 MPA
Poisson's Ratio
0.3
Density
1.1E-9
Results
Review the Contact Force Snap Fit Assembly.
Figure 2. Contact Force
Review the Deformation of Snap Fit Assembly.
Figure 3. Deformed and Un-deformed State of the Snap Fit Assembly
Review the Element Stress of the Snap Fit Assembly.
Figure 4. Element Stress Plots of the Snap Fit Assembly