This dataset contains geometries, simulations results, and experimental results used in the paper "UAV Icing: Aerodynamic Degradation Caused by Intercycle and Runback Ice".
The aim of the paper is to quantify the aerodynamic influence of intercycle and runback ice using wind tunnel tests and numerical simulations.
This dataset contains the clean wing geometry and the geometries of both intercycle ice shapes, the lift and drag coefficients as simulated numerically, and the force measurements from the wind tunnel tests.