Software Engineer, Engineering Applications

You will work closely with system owners across loads, flight dynamics, and structures to design and build the internal software backbone that enables multidisciplinary design optimization across the aircraft. Your tools will directly shape how we analyze, iterate, and converge on flight-ready hardware.

• Develop and maintain Python-based stress analysis templates, including composite plate buckling, classical laminate theory (CLT), and composite failure theory implementations
• Create and own a scalable loads database system that makes loads analysis data readily accessible to stress analysts and design teams
• Implement aeroelastic solution sequences as part of a custom-built loads analysis tool