Topology Optimization of a Drone
Application ID: 98661
Topology optimization for low volume fraction in 3D follows the same methodology as in 2D for medium volume fractions. The only difference is the need for iterative solvers. This model demonstrates topology optimization of a drone for a volume fraction of 12.5 %, while considering two load cases.
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® et
- Module Optimization et
- soit le Module MEMS, Module Multibody Dynamics, ou Module Structural Mechanics
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 Grille des Spécifications 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.