AirfoilMNIST is a dataset of two-dimensional, RANS-based flow fields for NACA 4- and 5-series airfoils. The dataset consists of around 148,000 simulations for Mach numbers up to 0.6 and angles of atta
Matlab code used to calculate numerically the area below the trajectories in the presence of air drag for the three animal species considered in this work (Fig. 4)
This dataset is associated with the thesis "Geometric Characterization of Aircraft Icing" (ISBN 978-3-947623-82-2) and includes geometries used to analyze aircraft icing on cowl lips during take-off a
