Closed hrobeers closed 5 years ago
@ehsanMa86 I'm wondering what you used this mesh for, laminar flow?
I'm far from a mesh independent solution using this mesh for the NACA0012 SA validation case https://turbmodels.larc.nasa.gov/naca0012_val.html
Without these improvements it's not even converging.
I will try to get this mesh closer to the NASA mesh.
@hrobeers Wow, this looks great! I merged your changes to the repository. Thanks for your contribution.
I didn't use this mesh for the CFD test cases. So I am short in answering to the question of the convergence of solution.
You're welcome, thanks for the great starting point ;)
I'm getting closer to a scalable and validated mesh, updates will follow later.
Thanks for improving it. It makes a huge difference.
Note: I'm still in progress of benchmarking and validating.
These changes do:
The images below illustrate the improvements. Note that the resolution is kept identical, this has no impact on skewness but is important when comparing BL refinement.
Full mesh skewness
Original: Improved:
Zoomed skewness
Original: Improved:
BL refinement (same number of cells)
Original: Improved: