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 IncludedParametric 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 SummaryWing-only CFD simulation performed

Lift at 8° AoA: ~370 N

Drag at 8° AoA: ~100 N

Aileron torque (20° deflection): ~80 Nm total (Z-axis)

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

Note on StabilityThis 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