AeroForge workspace

Structural Weight Estimation

Raymer class II weight estimation from geometry

Project

Units

Structural Weight Estimation

Raymer/Nicolai Class II semi-empirical weight estimation.

Wing

Span (m)

Area (m2)

Taper ratio

Sweep (deg)

t/c ratio

Fuselage

Length (m)

Width (m)

Tail

H-tail area (m2)

V-tail area (m2)

Performance

MTOW (kg)

Ultimate load factor

Cruise speed (m/s)

Landing Gear

Strut length (m)

Retractable