Composite Flap Static Analysis, courtesy of Triton Aerospace LLC
First Flight
Before First Off

Home Projects Triton A500

This project started by a request of Triton Aerospace LLC.

To optimize the weight of originally metal A500 (formerly Adam A500) structures the company decided to verify weight reduction due to application of composites.

The project implied to build finite element models of composite inboard and outboard sections of the flap and aileron and run their preliminary structural FE analysis.