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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. -
UIUC airfoil database
The UIUC airfoil database, containing nearly 1,600 real-world airfoil designs. -
Airfoil dataset
The Airfoil dataset contains aerodynamic and acoustic test results for airfoil blade sections in a wind tunnel. -
Non-linear case (124 RANS solutions)
A database of airfoil aerodynamic simulations used to train a convolutional autoencoder to predict aerodynamic stall. -
Linear case (33 RANS solutions)
A database of airfoil aerodynamic simulations used to train a convolutional autoencoder to predict aerodynamic stall.
