About

Built for people who build flying hardware.

An independent aerospace engineering studio. Runs locally — your geometry stays on your machine.

Nicholas Liautaud — Founder of AeroForge
Founder & Lead Engineer

Nicholas Liautaud

Aerospace engineer · Founder, AeroForge

I started AeroForge because the tools I needed didn’t exist in one place. I’d be modeling an airfoil in XFOIL, then a sectional in AVL, then doing weight & balance in a spreadsheet, then opening OpenFOAM for a sanity CFD pass — and every transition lost information. AeroForge is the workspace I wanted: every analysis on the same geometry, the same units, and the same source of truth.

I build things end-to-end — airframes, solvers, software, and the UI on top of them. I care about results that hold up to a wind tunnel, not screenshots that look good on a slide.

5
engineering surfaces shipped
1
person, full-stack
user-license cost

Background

A decade building airframes and wiring solvers by hand. Too much engineering time burned at the boundary between tools instead of inside them. AeroForge is the workspace I wish I'd had on day one.

What I've built

Not a slide deck — the fourth attempt at this problem, first one that works.

flagship

AeroForge

Five surfaces, end-to-end, one engineer.

pipeline

XFOIL + OpenFOAM

One geometry from 2D polar to 3D RANS.

desktop

Offline app

Runs in a hangar without wifi.

hardware

Real airframes

Used on actual airframes. Not academic.

What we believe

01

Owned, not rented.

Runs locally. No subscription. No cloud lock-in.

02

Integrated beats best-in-class.

Five surfaces, one workspace, one geometry.

03

Industry solvers, not toys.

XFOIL and OpenFOAM when available. Analytical fallback otherwise.

04

Speed is a feature.

Polars in seconds. Trim instantly. CFD as fast as your mesh.

Under the hood

A real engineering stack. Not a chatbot wrapper.

Aerodynamics
  • XFOIL viscous polar (Drela, MIT)
  • Analytical thin-airfoil fallback
  • Reynolds & Mach sweeps
Mass & balance
  • Composite CG & %MAC
  • Neutral-point & static-margin solve
  • Envelope & loading-case checks
Stability & control
  • AVL-equivalent derivatives
  • Cm-α, Cn-β, dihedral effect
  • Lift-curve slope, control authority
Flight mechanics
  • Steady level trim (L = W)
  • α, CL, L/D at operating point
  • Weight / altitude / airspeed walkers
CFD
  • OpenFOAM steady RANS
  • STL geometry intake
  • Analytical preview when offline
Delivery
  • Next.js web workspace
  • pywebview offline desktop build
  • FastAPI Python backend

Open the workspace.

Five surfaces. One geometry. No subscription.