UAV Concept V1 is a fixed-wing unmanned areal vehicle concept designed in Fusion 360. The design includes a streamlined fuselage, taped wings, V-tail, pusher propellor configuration, nose sensor turret, and underwing payload mounting points. This project focuses on: -Aircraft CD design -UAV configuration development -Aerodynamic geometry -Engineering documentation
-Design a complete UNV concept model -Practice aircraft CAD modelling in Fusion 360 -Apply basic aerospace design thinking -Prepare a portfolio-ready engineering project
|Parameter | Value| |Wingspan | 1900mm| |UAV Length, nose to Propellor | 1280 mm| |Wing chord | 190 mm| |Wing Area | 0.361 m^2| Aspect Ratio | 10 |
-Fixed-wing UAV -Rear Pusher propellor -V-Tail Configuration -Nose sensor turret -Aspect ratio
-Autodesk Fusion 360
##Project Files -Cad files in '/CAD' -Images in '/images' -Drawings in '/Drawings' -Calculations in '/Calculations' -Report in '/Report'
Current stage: Concept Design Future Work:
-Mas estimation -Propulsion Sizing -Stability analysis -Flight simulation -Structural analysis