wouah thanks for the video it is one of the best ansysfluent video i watched

Hi LEAP Australia, I am trying to simulate flow over an airfoil NACA0012 . I have made the grid with 40693. But when I am trying to simulate it in Fluent First thing it gives me a warning: The mesh contains very high aspect ratio hexahedral or polyhedral cells. The default algorithm used to compute the wall distance required by the turbulence models might produce wrong results in these cells. Please inspect the wall distance by displaying the contours of the 'Cell Wall Distance' at the boundaries. If you observe any irregularities we recommend the use of an alternative algorithm to correct the wall distance. Please select /solve/initialize/repair-wall-distance using the text user interface to switch to the alternative algorithm. Thanks

How u calculated the drag,lift coefficient from the plot , if u press on compute it is showing the last value but it is not correct , how u calculated the average?????

Please can you tell me why you have deleted connexions in 4:41 ? Thanks you very much for the help