OA
ReadyOpenFOAM airfoil aerodynamic validation
An OpenFOAM v2606 NACA 0012 validation study at Reynolds number 6 million, covering three meshes, seven angles, lift, drag, surface pressure, wall resolution, and NASA comparison.
- OpenFOAM v2606
- Python 3
- Matplotlib
Software compatibility
OpenFOAM v2606 onlyCases are prepared for the OpenCFD OpenFOAM v2606 distribution. No ANSYS Fluent, COMSOL, STAR-CCM+, or OpenFOAM Foundation v14 files are included.
- Project ID
- GP-AE-1LLG1AK
- Domain
- Aerospace
- Complexity
- Advanced
- Software
- OpenFOAM v2606 only
- Catalogued
- 22 Aug 2026
- Licence
- Single buyer
- Repository
- Private handover
- Buyer record
- Never public
Included in the project
- Programmatic NACA 0012 geometry and circular O-grid workflow
- Three mesh levels with 2,688, 5,760, and 10,752 cells
- Eleven completed steady RANS cases from -4 to 15 degrees
- Lift, drag, moment, Cp, y+, residual, and mesh-quality evidence
- NASA numerical comparison at 0, 10, and 15 degrees
- 17 labelled figures in PNG and SVG with raw JSON and CSV results
- Complete project files, models, calculations, and analysis material in a private GitHub repository
- 80-page project documentation in PDF and editable Word formats
- 9-page setup and usage guide