What is it about?

Adaptive mesh solutions from several flow solvers, error estimates and adaptive meshing packages are compared on a 2d high-lift airfoil application. All methods show mesh convergence to very similar results. Differences in convergence efficiency are examined to provide recommendations for future adaptive mesh applications.

Featured Image

Read the Original

This page is a summary of: Comparing Unstructured Adaptive Mesh Solutions for the High Lift Common Research Airfoil, AIAA Journal, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060088.
You can read the full text:

Read

Contributors

The following have contributed to this page