AeroForge workspace

Stability & control

AVL-equivalent derivatives. CG, NP, static margin, Cm-α, Cn-β, dihedral effect.

Project

Units

Defaults match a typical LSA. Tweak the wing if you need to, then hit Compute. Tails, parts (CG), and CG envelope have sensible defaults — open the disclosures only if you want to override.

Wing

Span (m)

Root chord (m)

Tip chord (m)

1/4-c sweep°

x root LE (m)

Incidence°

Dihedral°

Horizontal tail (included, defaults)

include horizontal tail

Span (m)

Root chord (m)

Tip chord (m)

1/4-c sweep°

x root LE (m)

Incidence°

Dihedral°

Vertical tail (included, defaults)

include vertical tail

Span (m)

Root chord (m)

Tip chord (m)

1/4-c sweep°

x root LE (m)

Incidence°

Dihedral°

Parts (CG) — 6 items, total 464 kg

CG envelope — fwd 15% / aft 35% MAC

Fwd limit %MAC

Aft limit %MAC

Flight condition — 50 m/s @ 0 m (dynamic modes ON)

compute dynamic modes & rate derivatives at this operating point

Velocity (m/s)

Altitude (m)

Results

Fill the layout and hit compute. Numbers, then derivatives.

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