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A CFD study on aerodynamic characteristics of a middle wing for WIG catamaran during ground effect

Priyanto, Agoes and Abd Malik, Adi Maimun and S., Jamei and I., Suharyanti (2010) A CFD study on aerodynamic characteristics of a middle wing for WIG catamaran during ground effect. In: 10TH ASIAN INTERNATIONAL CONFERENCE ON FLUID MACHINERY, 2010, Kuala Lumpur, Malaysia.

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Official URL: http://dx.doi.org/10.1063/1.3464942


In this paper the influence of ground effect on the aerodynamic character of NACA 6409 were numerically studied. The simulations of the wing were performed by three dimensional Computational Fluid Dynamic (CFD). The important aerodynamic characters such as lift and drag coefficient, lift to drag ratio were determined with variation in some principle aerodynamic parameter, for instance the angle of attack and aspect ratio. The ground clearance ( h/c ) in CFD simulation was 0.1. This simulation showed that there was enhancement on lift coefficient and reduction on drag coefficient related to incremental of aspect ratio when a aircraft flying in proximity to the ground. The ?-e turbulent model was used in CFD model. Numerical results were compared with experimental data of another researcher. As a application of this CFD simulation was calculating the lift-drag coefficient and lift to drag ratio from middle wing of WIG Catamaran.

Item Type:Conference or Workshop Item (Paper)
Uncontrolled Keywords:aerodynamics, vortexes, turbulent flow, reynolds number; aerodynamics, vortex dynamics, turbulence simulation and modeling, high-reynolds-number turbulence
Subjects:T Technology > TJ Mechanical engineering and machinery
Divisions:Mechanical Engineering
ID Code:27118
Deposited By: Mrs Liza Porijo
Deposited On:27 Jul 2012 07:21
Last Modified:07 Feb 2017 07:27

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