NACA 0012 airfoil dataset

The dataset used in this paper is a high-dimensional aerodynamic modeling problem of the NACA 0012 airfoil with 38 input parameters.

Data and Resources

Cite this as

Kai Cheng, Ralf Zimmermann (2024). Dataset: NACA 0012 airfoil dataset. https://doi.org/10.57702/qisqyd0j

DOI retrieved: December 16, 2024

Additional Info

Field Value
Created December 16, 2024
Last update December 16, 2024
Defined In https://doi.org/10.1137/22M154315X
Author Kai Cheng
More Authors
Ralf Zimmermann
Homepage https://doi.org/10.1038/s41598-021-94444-4