On the basis of boundary layer with the airfoil profile, this research
attempts to investigate the effect of the angle of spread of the winged air
suction equipment on the efficiency of operation. The application of Fluent
with the split-middle method under the identical operation mode is expected
to optimize the spread angle. The investigated airfoil profile is NACA6413,
of which the restrictions on the critical angle of spread suggested in
literature will be overcome through the interactions between the internal and
external flow fields. As a result, the air speed might increase. The wind
tunnel test employed in this research offers the solid evidences to support
this hypothesis. The test demonstrates that when the angle of spread is
larger than 12?, the effect of accelerating the air flow is still observable.
Following the optimization, the air suction effect of the equipment would be
optimal when its angle of spread reached 30?.