Wing Designer — Interactive Aerodynamic Design Tool

Scoring Class

Root

NACA Airfoil

Chord (ft)

Incidence (deg)

Re (1e6)46.095

Tip

NACA Airfoil

Chord (ft)

Incidence (deg)

Re (1e6)30.730

Wing

Span (ft)

Dihedral (deg)

Sweep (deg)

Taper Ratio0.6667

Geo. Twist (deg)0.00

Spanwise Panels

Chordwise Panels

Cruise

Velocity (kts)

AoA (deg)

Altitude (ft)

Density (kg/m³)0.493

Viscosity (kg/m-s)1.51e-5

Mach0.50

Wetted Area (S/S_ref)

Skin Fric. Cf

Empty Wt (lbf)

Engine

Prop Jet

SFC (lb/hp-hr)

Prop efficiency

TSFC (lb/hp-hr)

Wing fuel vol (%)

About

Web adaptation of Wing Designer, a MATLAB tool built at USMA by P. Root & J. Rogers.

Adapted by Claude Opus 4.6 and J. Baxter.

Output

Lift (lbf)--

Payload (lbf)--

Fuel Wt (lbf)--

Drag (lbf)--

Ind. Drag (lbf)--

Prof. Drag (lbf)--

Range (mi)--

Bend. Mom. (N-m)--

Wing Vol (ft³)--

Min. Struct. (lbf)--

Score --