To evaluate different design solutions given multiple multidisciplinary requirements?
To determine the propulsion system requirements for an innovative aircraft, e.g. with hybrid electric propulsion?
To calculate weight estimates for aircraft concepts?
To estimate the performance of novel aircraft concepts, e.g. in terms of environmental impact?
A long track record in aircraft multidisciplinary design and optimisation (MDO) including collaboration with international industrial and research partners
Conceptual design and sizing methodologies for conventional and (hybrid-)electric propelled aircraft
Corresponding efficient and integrated tooling: MUCH – MUltidisciplinary Conceptual design of Hybrid electric aircraft
Aircraft propulsion and mission modelling capabilities
