| 摘要 |
There is disclosed an aircraft wing rib 20 comprising a structural rib section 22 to which a wing skin 18 can be attached; and a suction conduit 34 to which, in use, a negative pressure can be applied so as to cause air to be drawn through suction holes 50 provided in the outer surface of the wing skin. There is also disclosed an aircraft wing 10 including such a wing rib. |
