Prediction of Aerodynamics Coefficients of Modified NACA 4415 Airfoil Using Computational Fluid Dynamics
The aim of the resent work is to predict the aerodynamic performance of modified NACA 4415 airfoil using computational fluid dynamics modelling. The performance is compared to that of NACA 4415 Standard. The simulation is performed using FLUENT with the variables of freestream velocity (i.e. 3, 4, 5...
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| Principais autores: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
EDP Sciences
2020-01-01
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| Series: | E3S Web of Conferences |
| Acceso en liña: | https://www.e3s-conferences.org/articles/e3sconf/pdf/2020/62/e3sconf_icenis2020_11002.pdf |
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