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For Educators · Airfoil Lift & Drag

Airfoil Lift & Drag for a wind-tunnel airfoil

Built for educators teaching it to a class. Drop a live demo into a lecture or assign it as a shareable link — no lab installs. Simulate a wind-tunnel airfoil live below — adjust the inputs and watch it respond, right in your browser.

Airfoil Lift & DragLive

Controls

Presets

Lift rises almost linearly with angle of attack — until the airflow separates and the wing stalls, losing lift sharply. Drag has a fixed part plus induced drag that grows with lift squared and shrinks with aspect ratio. The lift-to-drag ratio, peaking at a modest angle, is the single number that governs a wing's efficiency.

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Data Inspector

Lift coeff. CL0.53
Drag coeff. CD0.033
Lift/Drag16.0
Statusattached

Governing equation

Reading this result: Pre-stall: lift rises almost linearly with angle of attack at 6°, well below the ~15° stall angle. Adding camber would lift the entire curve higher.

Runs locally in your browser — free forever. Scale to the cloud when reality gets heavy.

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Frequently asked questions

Is this good for educators?
Yes — this version of "Airfoil Lift & Drag for a wind-tunnel airfoil" is framed for educators teaching it to a class. Drop a live demo into a lecture or assign it as a shareable link — no lab installs.
Do I need to install anything?
No. It runs in any modern browser, free, with no account required.