Mesh Independence in CFD: NACA2412 Example (Ansys Student) 

This is helped me out a ton. Cheers Cillian.

Thank you very much!! Such good quality and well-explained content is appreciated. Keep it up because it is really a great job and my sincere congratulations 👏👏

Awesome lecture and indeed a very helpful video...

How did you extracted the experimental data to plot the graph for Multi Variable GCI?

Thank you so much! Your videos have helped me a lot! Keep up the good work!

Thank you. Your files were really helpful.

Your videos are really helpful. Keep it up mate

Your videos azre very helpful!! However, I would like to ask you: Maybe you should change the bias factors??

G8 bruh, when is your next video coming, eagerly waiting for it

If you could make a lecture on airfoil design from scratch it would be great. Like the history of airfoil design till current design styles.

Good video.Could you please make a video that teaches how to simulate Drag coefficient of a soccer ball ? Thanks.

Thanks a million! ;)

Could you please make a video that teaches how to build the mesh for a 3D airfoil with vortex generators? Thanks.

Thanks

Great video 🎉

@20:02 Error Alert: The relation shown for phi_ext_21 should have (r**p - 1) in the denominator.

god sent

well done

How to plot any Cp vs X/C, while usually in Fluent we can have Cp vs X(m) data?

Good video❤

hello i was doing a project and conducting a baseline validation so as a part of that i am doing this mesh study , but i was advised to also do a domain study could u make a video for that or if i am confusing myself that mesh and domain study are the same , thanks , if anyone else can give some info aswell plz

And for non-constant grid refinement ratios?