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- W2386606369 abstract "Wind turbine performance is improved using numerical simulations of the NACA63 2 215 airfoil with a 45° flap and a Gurney flap by solving the compressible Reynolds averaged Navier Stokes equations employing the q ω turbulence model. The Navier Stokes and turbulence model equations are discretized using the new LU implicit scheme in time and the modified fourth order high resolution MUSCL TVD scheme in space. The predicted pressure coefficient distributions along the airfoil surface and the predicted lift coefficients are compared with experimental results at various attack angles ranging from 0°~30° . The predicted values agree well with the experimental results. The numerical simulations are also used to compare the separated flow field for the baseline airfoil and the airfoil with a flap at 12° angle of attack from to analyze the lift enhancement of the airfoil with a flap." @default.
- W2386606369 created "2016-06-24" @default.
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- W2386606369 date "2000-01-01" @default.
- W2386606369 modified "2023-09-25" @default.
- W2386606369 title "Numerical simulation of 2D airfoil lift enhancement with flaps" @default.
- W2386606369 hasPublicationYear "2000" @default.
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