


High-energy propeller blade containment
Safety verification for an Advanced Air Mobility vehicle: can a failed composite blade reach the passenger cabin? Blade failure at 1700 RPM, about 75 m/s at the tip.
- Refined failure criteria for the progressive break-up of carbon/epoxy skins and the crushing of the foam core
- Aluminium against composite shielding compared on absorbed energy; plastic strain up to 7.6 % in the containment wall
- Thousands of contact segments generated automatically for stable fragment-to-shield contact







