Minimum BS in Aeronautical Engineering or equivalent from an accredited institution with 7-10 years of experience working within an aerospace/defense multi-disciplinary environment working on aerodynamics, power and thermal management systems, mass properties, and other support vehicle performance and design modeling initiatives. Broad experience working with (CFD) Computational Fluid Dynamics, analysis in aerodynamics, mathematics, static load methods, and aircraft sizing & performance. Experience supporting wind tunnel tests and flight tests, performing validated CFD simulations to characterize both internal and external flows, and experience developing aerodynamic models for basic stability and control effectiveness.