04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
CLOSED-LOOP GUST LOADS ANALYSIS OF A SUPERSONIC FIGHTER AIRCRAFT
A. Voß¹, J. Baier¹; ¹DLR Institute of Aeroelasticity, Germany
Military supersonic fighter configurations, due to their high maneuverability requirements, are usually sized by maneuver loads. This work investigates if gusts can exert higher loads on the primary structure in terms of section loads and structural dynamic accelerations.