It includes:

✅ Wing surface with NACA 4412 airfoil

✅ Internal structure: spars, ribs, and stringers

✅ Control surfaces: flaps and ailerons

✅ Designed for modular spray integration and lightweight UAV construction

???? What’s Included
Parametric wing model (400 mm chord, rectangular planform)

Structural supports: dual main spars + ribs

Full-length flaps and ailerons with actuation cutouts

Designed for CFD, FEA, and aerodynamic optimization

???? Simulation Summary
✅ Wing-only CFD simulation performed

Lift at 8° AoA: ~370 N

Drag at 8° AoA: ~100 N

Aileron torque (20° deflection): ~198 Nm total (Z-axis)

Simulations show high lift at cruise (30 m/s), suitable for wide-area spraying

⚠️ Note on Stability
This file includes the wing only — fuselage and tail designs are not included.
If you plan to simulate static or dynamic stability, you’ll need to:

Design a fuselage pod

Establish a valid CG forward of the aerodynamic center

Optionally add horizontal stabilizers

???? Upcoming Release
Stay tuned for the full UAV assembly, including:

Fuselage pod with payload system

Boom-integrated spray mechanism

GPS & autopilot integration

Camera + mapping suite