Wing Designer

Score

Get Started

Wing design has a lot of parameters. Pick a real aircraft to start from, then tweak the sliders to see how each change affects the score.

Start from a real aircraft Choose one ▾

Scoring Class Heavy Transport ▾

Root Airfoil

NACA Airfoil 2412 ▾

Chord 1.0ft

Incidence 0.0deg

Reynolds (1e6) --

Tip Airfoil

NACA Airfoil 2412 ▾

Chord 1.0ft

Incidence 0.0deg

Reynolds (1e6) --

Wing Geometry

Span 10ft

Dihedral 0.0deg

Sweep 0.0deg

Taper Ratio --

Geometric Twist --

Spanwise Panels 10

Chordwise Panels 6

Cruise Conditions

Velocity 292kts

Angle of Attack 0.0deg

Altitude 28,000ft

Density -- kg/m³

Viscosity -- kg/m-s

Mach --

Wetted Area (S/S_ref) 7.0

Skin Friction Cf 0.0040

Empty Weight 83,000lbf

Engine

Engine Type

SFC 0.49lb/hp-hr

Prop Efficiency 0.85

TSFC 0.69lb/hp-hr

Wing Fuel Volume 25%

Results

Lift (lbf)--

Payload (lbf)--

Fuel Wt (lbf)--

Drag (lbf)--

Ind. Drag (lbf)--

Prof. Drag (lbf)--

Range (mi)--

Bend. Mom.--

Wing Vol (ft³)--

Min. Struct. (lbf)--

Score --

Wing View