What you get: shaft power, Cp, torque, tip-speed ratio, power curve versus wind speed, blade geometry — computed by Heliciel.
→ About the Heliciel MCP connector
→ Install in Claude
→ Get an MCP pass
→ Wind turbine blade tutorial
→ Wind turbine power and wind speed
→ Version française
Wind turbine power calculation with ChatGPT or Claude
With the Heliciel MCP connector, your AI assistant computes the power harvestable by a wind turbine from diameter, blade count and wind speed, plots its power curve, optimizes its RPM and exports the blades. The power coefficient Cp, tip-speed ratio and torque are those of Heliciel's BEM (Blade Element Momentum) computation, not the Betz formula with a "typical" efficiency.
The problem: Cp depends on the blade, not only on the wind
Everyone knows P = ½ ρ A V³ Cp; what nobody knows offhand is the Cp of your rotor at your RPM. It results from the blade geometry (twist, chords, airfoils), the tip-speed ratio and the polars at the local Reynolds numbers. A language model alone answers "Cp ≈ 0.35 to 0.45": an interval, not a computation. Heliciel computes the Cp of the actual blade by blade element theory applied to energy-capturing rotors.
Real dialogue: 3 blades, 4 m, 8 m/s wind
Real session in ChatGPT web (from the demo video).
"Load a wind turbine, 3 blades, 4 m diameter, 8 m/s wind — what power can I harvest?"
Heliciel loads the turbine_eolienne model and returns: tip-speed ratio 4.712, Cp 0.426, shaft power 1,528.94 W, torque 81.11 N·m. 0 errors, 0 warnings."Sweep the wind from 3 to 15 m/s."
The assistant first asks the method question: off-design (geometry and RPM fixed, what a real turbine undergoes) or redesign (optimal blade at every speed, what an ideal turbine could reach). The user answers "Off-design".
The chart is plotted by Heliciel and passed as-is ("Computed by Heliciel — not AI-generated").
13 points from 3 to 15 m/s, geometry and 180 rpm fixed.And with RPM optimization
On the same rotor, the request "Optimize efficiency" (method asked to the user before the call) returned during the validation campaign a Cp of 0.575 at 250 rpm, against 0.426 at 180 rpm: the tip-speed ratio was too low for this blade. Exactly the kind of question a rule of thumb does not settle.
Rotor export
"Export the propeller as STL": complete rotor with hub, 148.8 MB, link valid 60 minutes. The long export returns milestones; the assistant checks completion before giving the link.What you can ask next
- Design the blade for a given site (rated wind, diameter, generator RPM) rather than loading a model: Heliciel computes the optimal twist and chords.
- Compare 2 and 3 blades, or two diameters, at the same wind.
- RPM × wind map to choose the control law of a variable-speed generator.
- Hydrokinetic turbine: same approach in water, with cavitation check (hydrokinetic turbines).
- Export the blades as STL/IGES and the sections as JSON for manufacturing.
Limits specific to wind turbines
- Steady, ideal BEM: no atmospheric turbulence, wind shear or dynamic stall.
- No blade structural computation or extreme loads (storm); no dB(A) acoustics.
- The power returned is at the shaft: generator and drivetrain efficiency to be deducted.
Connect
- Get a Heliciel MCP pass on mecaflux.com.
- In Claude: connectors directory. Elsewhere: MCP connector at
https://mcp.heliciel.com/mcp(per-client details). - Authorize with the pass key, then describe your turbine and your wind.
Frequently asked questions
Why is the power negative at 3 m/s?
Because the RPM is fixed at 180 rpm: at low wind the tip-speed ratio becomes too high, the blade drags more than it harvests. A real turbine would slow down. Ask for a sweep at constant tip-speed ratio to see the other behaviour.
Does a Cp of 0.575 exceed the Betz limit?
No: the Betz limit is 0.593. But 0.575 is an ideal theoretical BEM Cp (smooth surfaces, no drivetrain losses); a real machine will be below. Heliciel states it and the connector reports it.
Can I reproduce these figures?
Yes: same model, same wind, same RPM give the same result.
Related pages: Heliciel MCP (overview) · drone propeller by AI · aircraft propeller by AI


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