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Unsteady aerodynamic forces of a flapping wing

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Figure

Fig.·∆τupstroke. Reynolds number 9. Vorticity plots at half-wing length at various times during one cycle
Fig.·(A) Non-dimensional angular velocity of pitching rotation (azimuthal rotation ((14
Table 4. Effects of stroke amplitude (Φ) on mean lift (CL) anddrag (CD) coefficients
Table 6. Data of free hovering flight and lift coefficient needed for weight support

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