Optimization of a Variable-Stiffness Composite Plate with a Central Hole
Application ID: 144551
This example demonstrates the optimization of fiber orientation in a variable angle tow (VAT) laminate to maximize stiffness under prescribed loading and boundary conditions. The composite laminate consists of a single layer of carbon–PEEK composite with transversely isotropic material properties.
The model showcases how curvilinear fiber paths can be used in a square plate with a central hole to achieve tailored stiffness and improved structural performance under specified loading conditions.
This model example illustrates applications of this type that would nominally be built using the following products:
however, additional products may be required to completely define and model it. Furthermore, this example may also be defined and modeled using components from the following product combinations:
- COMSOL Multiphysics® and
- Composite Materials Module and
- Optimization Module and
- either the MEMS Module, or Structural Mechanics Module
The combination of COMSOL® products required to model your application depends on several factors and may include boundary conditions, material properties, physics interfaces, and part libraries. Particular functionality may be common to several products. To determine the right combination of products for your modeling needs, review the Specification Chart and make use of a free evaluation license. The COMSOL Sales and Support teams are available for answering any questions you may have regarding this.
