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Run 2D airfoil geometry, meshing, CFD solving, and visualization through MCP.
Copy the install command and let the AI configure it · recommended for beginners
No copy-paste install info for "MCP-Server-for-CFD" yet — see the docs or source repo.
Use MCP-Server-for-CFD to create a 2D NACA 2412 airfoil, run meshing and CFD solving under a given freestream velocity and angle of attack, and return lift, drag, and pressure distribution visualizations.
Returns the airfoil geometry, computational mesh, aerodynamic coefficients, and pressure distribution visualizations.
Run CFD analysis for the same 2D airfoil at 0, 5, and 10 degrees angle of attack, summarize lift and drag results for each case, and generate comparison plots.
Provides a multi-case aerodynamic summary table and comparison charts for lift and drag.
Generate a computational mesh for a specified 2D airfoil, show mesh details, run a basic CFD case, and output velocity and pressure contour plots to inspect flow quality.
Returns mesh visualizations and velocity and pressure field plots for validating the simulation setup.
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