Project manager - Oversaw different sub teams, managed project scope, and validated high level architecture leading the team to place 8th out of 104 at a national level.

Validated payload packaging design, center of mass location, wing/tail sizing, and fuselage design.

Performed FEA on wings under flight loads and validated with four-point bend tests reducing wing weight by 55%.

Created MATLAB take-off model for wing-loading and thrust to weight relationship for optimal flight performance.

Analyzed airfoil profile and incidence angle with xlfr5 to improve overall lift, aerodynamic center, and flight stability.

Determined optimal battery cell count for propeller/motor combo for maximized flight time and flight performance.

Performed weight and strength analysis of composite body reducing weight of fuselage by 50%.

Drove decisions for specified aerodynamic loads on vehicle.

Optimized design and performed DFM checks of aerodynamic package to meet required specifications.

Determined maximum load cases from lift and drag forces on complete aerodynamic package.