Aerofoil drag reduction by shape optimization

Published: 30 May 2020| Version 3 | DOI: 10.17632/428zsnnkmj.3
Contributor:
Isaac Mark Joseph Manasseh

Description

Aerofoil drag reduction by optimizing the frontal surface of the aerofoil.

Files

Steps to reproduce

Analyze the stagnation pressure, mark the coordinates. Introduce a protuberance in the frontal surface on the aerofoil.

Categories

Aeronautics, Aerospace, Aerodynamics, Computational Fluid Dynamics, Aeroacoustics

Licence