ANSYS Fluent 2024 R2 visualization bug

>> YOUR LINK HERE: ___ http://youtube.com/watch?v=UkTEiHuZ1uQ

Inviscid flow past a NACA 0006 airfoil at AoA=0 degrees. Some kind of modelled boundary layer (within the first layer mesh) is shown in the Results module, but not in Fluent. Please note that not only the minimum but also the maximum velocity values are different. • Visit this to know more: https://librepenzzzador.blogspot.com/...

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