| 摘要 |
An enhanced performance rotorcraft rotor blade system and methods are presented. A rotor blade (304) comprises an inboard blade portion (318), and at least one controllable surface (328) coupled to the inboard blade portion (318). The at least one controllable surface (328) is operable to improve a lift of the inboard blade portion (318) by altering an angle of attack of the inboard blade portion (318) independent of the rotor blade (304). |
