Professional Fixed-Wing UAV designed entirely in SolidWorks for engineering visualization, simulation, and Digital Twin applications.

This project features a lightweight aerodynamic airframe with a modular structure optimized for long-endurance missions and future prototype development. The design is suitable for CFD analysis, structural optimization, and educational aerospace projects.NACA 4412 airfoil1430mm wingspan250mm chord at rootwing area 33dm^2fuselage length 930mmAUW around 2.5kgprint with LW PLA and laminate with fiber glassSpecificationsFixed-Wing UAVFully Parametric CAD ModelDesigned in SolidWorksModular AirframeLightweight StructureSimulation ReadyDigital Twin ReadyOptimized for CFD & FEA AnalysisApplicationsAerial MappingEnvironmental MonitoringPrecision AgricultureInfrastructure InspectionResearch & DevelopmentEngineering EducationSoftwareSolidWorksANSYS FluentANSYS Mechanical