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- W1492098387 abstract "The unsteady, incompressible, and viscous flow over airfoil NACA0012 in plunge motion was analyzed by using the Navier-Stokes equation. We explored the optimal phase angle for thrust force and propulsive efficiency while the chord flexure amplitude is varied from 0.05 to 0.7 in the condition that reduced frequency and non-dimensional plunge amplitude were fixed. Throughout the parametric study on the phase angle and chord flexure amplitude, maximum thrust force is able to be achieved near at 0 degree in all given conditions, meanwhile, it is found that the optimal phase angle has dependency of chord flexure amplitude, which achieves higher performance compared to previous studies." @default.
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- W1492098387 date "2009-11-01" @default.
- W1492098387 modified "2023-09-23" @default.
- W1492098387 title "Parametric study of chordwise flexibility of airfoil in plunge motion" @default.
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