Study of the influence of protuberances in the trailing edge of airfoils and determination of their aerodynamic efficiency through CFD using Ansys Fluent ... : Estudio de la influencia de protuberancias en el borde de ataque de perfiles alares y determinación de su eficiencia aerodinámica mediante CFD en Ansys Fluent ...

• Main Authors: González, Angel, Hinojosa, Jorge
• Format: Text
• Language: Spanish
• Published: Barcelona : Scipedia 2019
• Subjects: Airfoil; lift; CFD; protuberances; Perfil aerodinámico; sustentación; protuberancias; Dewey Decimal Classification500 | Naturwissenschaften510 | Mathematik; Dewey Decimal Classification600 | Technik; Dewey; Jorobada; Ballena jorobada; Humpback Whale; Megaptera novaeangliae
• Online Access: https://dx.doi.org/10.15488/13533; https://www.repo.uni-hannover.de/handle/123456789/13643

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...