To get started, Alex imported the wing's CAD model into FEMAP and began setting up the simulation. The team defined the materials, loads, and boundary conditions, and then ran the analysis using NX Nastran.
The initial results showed some areas of concern, with high stress concentrations in certain regions of the wing. Alex and the team used FEMAP's advanced post-processing capabilities to visualize the results and identify potential design improvements.
To further enhance the analysis, Alex discovered SAToolkit, a software toolkit that provided additional functionality for working with finite element models. SAToolkit allowed the team to perform more advanced tasks, such as parametric studies and optimization, which helped them to refine the wing's design.
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