This repository contains the code used for simulations in the study by Aksnes et al. (2023)
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Updated
Jan 25, 2024 - MATLAB
This repository contains the code used for simulations in the study by Aksnes et al. (2023)
Discrete vortex method codes for calculating lift coefficient of thin lifting airfoils
Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)
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