Create a 2D Mesh for airfoil section with ICEM скачать в хорошем качестве

Create a 2D Mesh for airfoil section with ICEM

Mesh for NACA4418 CFD ICEM, Ansys, CFD --- How to get the profile points Profile obtained from http://airfoiltools.com/airfoil/detai..., modified to match the format of ICEM. It's like a CSV with tabs instead of commas, and the first row defines the number of points. My file had 50 points, 25 above chord and 25 below chord, so 25 points two times. Therefore, the first line is: 25{tab}2. Then, x{tab}y{tab}z points, starting and ending with (1.0, 0.0), and duplicating the (0.0, 0.0) point, like this: 25 2 1.000000 0.000000 0. 0.996088 0.003332 0. 0.983662 0.007633 0. ... Since I want 25 points above, and 25 points below, my file should have 51 lines including the first header line. Export Then to export the mesh, click export at the right, select in the popup what program you will use later with that mesh, in my case it's fluent, and then click export to save to a file.