I need an Ansys Fluent Expert
Budget: $30 – $250 USD
I need to simulate an airfoil NACA 64-212
1. To calculate Cd and Cl.
2. Workbench containing the mesh solver setup.
3. Grid Convergence study (find attached template).
You can see the 2 attached files to know what is required.
Thank you
1. To calculate Cd and Cl.
2. Workbench containing the mesh solver setup.
3. Grid Convergence study (find attached template).
You can see the 2 attached files to know what is required.
Thank you