Study of the influence of protuberances in the trailing edge of airfoils and determination of their aerodynamic efficiency through CFD using Ansys Fluent
In the present research, the effect of incorporating protuberances in the leading edge to the aerofoil NACA-0012 was studied. For the simulations, two profiles were designed: parametric profile (NACA 0012) and modified profile (0012-MOD), with help of CAD Program Inventor Professional 2016. The 0012...
Main Authors: | , |
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Format: | Article in Journal/Newspaper |
Language: | Spanish |
Published: |
Barcelona : Scipedia
2019
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Subjects: | |
Online Access: | https://www.repo.uni-hannover.de/handle/123456789/13643 https://doi.org/10.15488/13533 |