Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes

This work focuses on a multidisciplinary design optimization of an aircraft wing. Among others, a structural optimization of the wing stiffness is performed. For a certain stiffness model, a set of relevant load cases can be determined that have high chance to cause active constraints. The purpose of this research is to investigate if the set of...