WingDesignerBeta

Wing Parameters

Aircraft Type

Span (m)

Root Chord (m)

Tip Chord (m)

Sweep Angle (°)

Twist Angle (°)

Dihedral Angle (°)

Airfoil Type

3D Wing Visualization

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Wing PropertiesAnalysis

Wing Area: 20.00 m²; Reference Area

Mean Aerodynamic Chord: 1.50 m; MAC

Aspect Ratio: 64.80; AR = b²/S

Taper Ratio: 0.33; ct/cr

Wing Volume: 4.00 m³; Approximate

Estimated Mass: 100.0 kg; Based on Volume

Aerodynamic Coefficients

Angle of Attack (°)

Lift Coefficient (CL): 0.000; at 0° AOA

Drag Coefficient (CD): 0.0000; Total Drag

Moment Coefficient (CM): 0.000; About MAC

Lift-to-Drag Ratio: 0.0; Efficiency