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Fig. 5. Non-dimensional angular velocity of flip rotation
() and azimuthal
rotation () of (A)
hindwing and (B) forewing; (C) time courses of total vertical force
coefficient (CL) and (D) total thrust coefficient
(CT) in one cycle.
) and azimuthal
rotation (
) of (A)
hindwing and (B) forewing; (C) time courses of total vertical force
coefficient (CL) and (D) total thrust coefficient
(CT) in one cycle.