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- W3178454953 abstract "In hydrofoil ship projects, it is important to choose the foil profile that provides the higher lift and the smaller drag minimizing the risk of cavitation. Moreover, hydrofoil ships have a higher drag on low speeds than conventional ships, highlighting the importance of low speeds analysis of the profile. This paper analyses 2212, 2309 and 4712 NACA profiles, used for hydrofoil applications, through bidimensional panel theory using the software XFOIL, and through bidimensional RANS equations and finite volume method using ANSYS FLUENT, with the objective to determinate the lift and drag coefficients for low Reynolds number. The analysis ranges from 0 to 15 degrees of attack angle, using a step of 2.5 degrees. The validation of the mesh for the finite volume method was made using experimental data from the E387 profile. According to the results obtained, the 4712 NACA profile has the highest lift-drag coefficient among the studied profiles." @default.
- W3178454953 created "2021-07-19" @default.
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- W3178454953 date "2021-07-08" @default.
- W3178454953 modified "2023-09-27" @default.
- W3178454953 title "Hydrofoil profile numerical analysis for low Reynolds number" @default.
- W3178454953 doi "https://doi.org/10.1201/9781003216599-8" @default.
- W3178454953 hasPublicationYear "2021" @default.
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