• Simulated expected static-loading cases to develop specifications for UAV then designed and implemented structural analysis experiments to verify them• Utilized FEA with multiple load cases on many components and materials to optimize stiffness vs weight• Developed various load-balance tests to measure rotor’s performance• Designed and built frame and landing gear to meet UAV’s high dynamic loads and a custom cowling for good aerodynamic performance while minimizing weight and keeping a high safety factor• Reduced cost by finding and utilizing market alternatives for custom applications• Data analysis and manipulation in LabView of cyclorotor air-flow data using sensors• Managed ~50% of total project load throughout design, fabrication, and installation stages and achieved it within a tight project deadline• Worked with contractors to design and fabricate custom carbon fiber cowling