Finite-element model of the aircraft structure – dynamic analysis of the wing
Finite-element model of the aircraft structure – dynamic analysis of the wing
Among other things, the structural behaviour of the aircraft was investigated during the project. This showed that the dynamic structural behaviour changes due to the propulsion units being distributed across the span of the wings. For example, the initial flexing of the wing is reduced quite considerably.
Credit: DLR (CC BY-NC-ND 3.0)