PPolySim OS

Pitot-Tube Airspeed

Aircraft measure speed from air pressure, not a speedometer. See how dynamic pressure becomes airspeed — and why true airspeed climbs with altitude.

Pitot-Tube AirspeedLive

Controls

Presets

A pitot tube measures the pressure difference between still and moving air, then airspeed follows from v = √(2Δp/ρ). Because air thins with altitude, true airspeed exceeds the indicated value up high — a key gotcha in aviation. Educational tool.

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Data Inspector

Air density1.225 kg/m³
True airspeed49.5 m/s
Indicated airspeed49.5 m/s
Mach number0.145

Governing equation

Reading this result: Near sea level the air is close to standard density, so true airspeed and indicated airspeed nearly coincide — the gauge reads reality directly.

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

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How it works

A pitot-static system measures dynamic pressure Δp, and airspeed follows from v = √(2Δp/ρ). Because air density falls with altitude, the same Δp corresponds to a higher true airspeed up high than the indicated value — a crucial distinction in aviation. Educational tool.

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The math, the assumptions, real-world uses, or a code translation — explained for this exact simulation.

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Frequently asked questions

Is this pitot tube airspeed calculator tool really free?
Yes. Pitot-Tube Airspeed runs entirely in your browser using your device's own compute, so local use is free forever. You only pay Compute Tokens if you scale a job to the cloud.
Do I need to install anything?
No. Everything runs client-side in a modern browser — no downloads, no license, no account required to start.
Can I save or share my simulation?
Create a free account to save projects, and use a shareable embed or minted DOI to publish a live, interactive version anywhere.
How accurate are the results?
The solver uses established numerical methods, but results are for research and educational purposes and should be validated against experiment or professional review before you rely on them.