04.2 - Structural Analysis and Design, Structural Dynamics, AeroelasticityVIRTUAL AIRCRAFT MODEL FOR AEROELASTIC SIMULATION AND LOAD PREDICTION OF A HIGH ASPECT RATIO COMPOSITE SWEPT WINGA. Hermanutz¹, M. Hornung¹; ¹Technical University of Munich, Germany To investigate the aircraft behavior including elastic effects, an aeroelastic virtual aircraft model of a civil transport aircraft with model reduction methods for load prediction is presented. In different transient flight maneuvers, critical load conditions are identified and used for detailed structural sizing. |