Fig. 12. The effects of rotation duration (
r) on force
coefficients. (A) Non-dimensional angular velocity of pitching rotation
(
) and azimuthal
rotation (
); (B) time
courses of lift coefficient (CL) and (C) drag coefficient
(CD) in one cycle. Reynolds number (Re)=200,
stroke amplitude (
)=150° and mid-stroke angle of attack
(
m)=40°; symmetrical rotation.