Aircraft wing architecture optimal assembly

The internal architecture of an aircraft wing contains many different systems and elements. The objective of this CFP is to deliver a design platform capable of assessing the volume and shape of the individual systems, the connections between them and other constraints within the internal wing space in order to provide a set of optimal assemblies that minimizes the overall volume. These optimal architectures should be able to integrate with the MISSION system design platform and be informed by the physics-based constraints coming from the dynamic models. Please refer to the full topic descriptions document published in this call.