Professional paper
https://doi.org/10.7225/toms.v10.n02.012
Investigation of Numerical Hydrodynamic Performance of Deformable Hydrofoil (Applied on Blade Propeller)
Noh Zainal Abidin
; Universiti Pertahanan Nasional Malaysia, Kuala Lumpur, Malaysia
Cédric Leblond
; Naval Group / Ecole Centrale de Nantes, France
Mohd Najib Abdul Ghani Yolhamid
; Universiti Pertahanan Nasional Malaysia, Kuala Lumpur, Malaysia
Mohamad Abu Ubaidah Amir Abu Zarim
; Universiti Pertahanan Nasional Malaysia, Kuala Lumpur, Malaysia
Farizha Ibrahim
; Universiti Pertahanan Nasional Malaysia, Kuala Lumpur, Malaysia
Ameer Suhel
; Universiti Pertahanan Nasional Malaysia, Kuala Lumpur, Malaysia
Abstract
The hydrofoil is a hydro-lifting surface that significantly contributes to marine transportation such as a boat, ship, and submarine for its movement and maneuverability. The existing hydrofoils are in fixed-shaped National Advisory Committee for Aeronautics (NACA) profiles, depending merely on the variation of Angle of Attack (AOA) such as rudder, hydroplane, and propeller blade. This research is concerned with the deformable hydrofoil that aims at modifying its NACA profile rather than its AOA. However, there is still a lack of knowledge about designing an appropriate deformable hydrofoil. Therefore, a numerical investigation of hydrodynamic characteristics for selected hydrofoils was conducted. After undergoing the 2D numerical analysis (potential flow method) at specific conditions, several NACA profiles were chosen based on the performance of NACA profiles. NACA 0017 was selected as the initial shape for this research before it deformed to the optimized NACA profiles, NACA 6417, 8417, and 9517. The 3D CFD simulations using the finite volume method to obtain hydrodynamic characteristics at 0 deg AOA with a constant flow rate. The mesh sensitivity and convergence study are carried out to get consistent, validated, and reliable results. The final CFD modeled for propeller VP 1304 for open water test numerically. The results found that the performance of symmetry hydrofoil NACA 0017 at maximum AOA is not the highest compared to the other deformed NACA profiles at 0 deg AOA. The numerical open water test showed that the error obtained on K.T., K.Q., and efficiency is less than 8% compared to the experimental results. It shows that the results were in good agreement, and the numerical CFD setting can be used for different deformed profiles in the future.
Keywords
CFD; NACA; Numerical analysis; Hydrodynamic; Potential flow; Finite volume
Hrčak ID:
269860
URI
Publication date:
21.10.2021.
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