Structured O-type Grid Around NACA Airfoil
I'm trying to make a structured O-type grid around NACA airfoil. But I'm unable to do so as I don't know the exact values of biasing factor, number of elements etc. I have done the tutorial of Structured C-type mesh. https://imgur.com/8F2RORe
|
All times are GMT -4. The time now is 20:13. |