Mesh Independence in CFD: NACA2412 Example (Ansys Student)

In this video, I describe the grid convergence index method for mesh independence studies in CFD, and I go through a practical example of a NACA2412 airfoil in ANSYS student.

Files here: https://tinyurl.com/2p86ybrt

00:00 - 1:46 Intro

** Start of Lecture **
2:27 - 7:19 - Verification and Validation
7:19 - 9:02 - How to conduct a Mesh Independance Study
9:02 - 14:54 - Grid Convergence Index Method Intro
14:54 - 22:52 - Grid Convergence Index Method Steps

** Start of Tutorial **
22:52 - 29:15 - Improving Mesh Quality of my old file
29:15 - 41:54 - Coarse Mesh Study
41:54 - 43:20 - Medium, Fine
43:20 - 53:20 - GCI for Lift, Drag
53:20 - GCI for Pressure Coefficient

Enjoy :)

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