
Formula SAE · Structural design September — November 2025
Topology-Optimized Front Wing Mount
I rebuilt the front-wing frame mount around new chassis hard points, used topology optimization to remove inefficient material, and verified the manufacturable result under a 150 lbf vertical load.
- Role
- Design and analysis
- mass reduced
- 72 → 67 g
- final peak displacement
- 0.34 mm



