03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
THE ACTIVE AEROELASTICITY CONCEPT - THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT
G.A. Amiryants, Russia; A.V. Grigorev, Russia; Y.A. Nayko, Russia; S.E. Paryshev, Russia
As development of Active Aeroelasticity concept results of theoretical and experimental investigations of spiroid winglet with forward and rear tip aileron shifted with respect to the wing elastic axis are presented. Also effectiveness of differential leading edge control for advance passenger aircraft with high aspect ratio swept wing are demonstrated