Problem

Traditional UAV prototyping is costly and time-consuming, relying on physical build-test-crash cycles that slow down iteration and increase expenses.

Solution

Developed a parametric flying-wing UAV design in SolidWorks, integrated with Star-CCM+ and HEEDS for automated optimization of wing geometry (span, twist, sweep). Conducted a preliminary airfoil analysis using XFLR5 and aerodynamic and stability analyses and Design Manager, then created MATLAB state-space model to assess flight stability. Optimized structural design in AN SYS Mechanical for manufacturability and material efficiency.

Impact

Completed a validated UAV prototype in 3 months-significantly reducing development time and cost compared to standard methods­while creating a reusable, automated workflow adaptable to future UAV models.