Dataset Groups Activity Stream 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. BibTex: @dataset{Kai_Cheng_and_Ralf_Zimmermann_2024, abstract = {The dataset used in this paper is a high-dimensional aerodynamic modeling problem of the NACA 0012 airfoil with 38 input parameters.}, author = {Kai Cheng and Ralf Zimmermann}, doi = {10.57702/qisqyd0j}, institution = {No Organization}, keyword = {'aerodynamics', 'airfoil', 'engineering'}, month = {dec}, publisher = {TIB}, title = {NACA 0012 airfoil dataset}, url = {https://service.tib.eu/ldmservice/dataset/naca-0012-airfoil-dataset}, year = {2024} }