1
Failure Analysis: The Need for Internal Structure
To understand the necessity of a robust internal skeleton, I analyzed the failure points on last year's front wing. The absence of proper internal structuring led directly to catastrophic skin failure.
Previous Manufacturing Flaws
The original design featured relief cuts in the carbon fiber front wing that acted as stress concentrations. These cuts were made to ease manufacturing, but they created significant weak points in the skin.
The Y-Axis Moment Failure
Further analysis revealed that the wing cracked because there was no internal spar designed to handle the moment in the Y-axis. The out-of-plane forces from steering and cone strikes overloaded the skin plies, which naturally failed at the manufacturing relief cuts.
