Aerofoil drag reduction by shape optimization
Published: 30 May 2020| Version 3 | DOI: 10.17632/428zsnnkmj.3
Isaac Mark Joseph Manasseh
Aerofoil drag reduction by optimizing the frontal surface of the aerofoil.
Steps to reproduce
Analyze the stagnation pressure, mark the coordinates. Introduce a protuberance in the frontal surface on the aerofoil.
Aeronautics, Aerospace, Aerodynamics, Computational Fluid Dynamics, Aeroacoustics