Error in solving compressible NS equation with NACA airfoil
******************* This email originates from outside Imperial. Do not click on links and attachments unless you recognise the sender. If you trust the sender, add them to your safe senders list https://spam.ic.ac.uk/SpamConsole/Senders.aspx to disable email stamping for this address. ******************* Hi all, I am trying to study compressible flow over a NACA airfoil with Nektar++ and I am seeing a Segmentation fault while running the simulation. The steps for creating the simulation are as follows: 1. Create mesh in GMSH (File attached) 2. Convert GMSH to Nektar++ compatible format using NekMesh 3. Setup the session file as per problem statement (Session file attached). [image: image.png] I would appreciate any help that I can get with this in trying to understand the source of this error. -- Thanks Varun
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Kumar, Varun