Project
UAV Aerodynamic & Structural Optimization
Technology
SolidWorksAerodynamic OptimizationCFD AnalysisUAV DesignAircraft StructuresFlight Stability Analysis3D PrintingFDM ManufacturingStructural OptimizationLightweight DesignAvionics IntegrationPrototype ManufacturingSystem Integration
Year
2023
Context
Aerodynamic optimization and development project for a high-performance UAV platform, addressing efficiency, stability, and lightweight manufacturing for reliable aerial operation.
Constraints
The aircraft configuration had to hit an 18% static margin to balance longitudinal stability and maneuverability, using a trapezoidal wing (1800 mm span, 0.5 taper ratio) with Hoerner winglets, validated by CFD simulation.
My Role
Aerodynamic and structural performance simulation and optimization: CFD validation of the wing configuration, and structural design of the fuselage combining FDM 3D printing, sandwich panel construction, and Gyroid infill optimization, with reinforced high-stress areas (motor mounts, landing gear attachments).
