Abstract: Provided is a multi-element rotor blade, including a primary element and at least one complimentary element, each having an aerodynamic profile. The primary element is joined by fastening elements to the at least one complimentary element such that the at least one complimentary element is adjacent to the primary element in a chordwise direction perpendicular to an axis of rotation of the blade and perpendicular to a longitudinal length of the blade. The at least one complimentary element is disposed closer to a blade root end of the primary element than to an opposite end of the primary element.