Services

Conceptual and preliminary design support for novel civil aircraft, including hydrogen and electric propulsion systems.

Physics-based structural sizing of wings, struts, and trusses for moderate to high aspect ratio configurations.

Parametric and optimisation studies for strut- and truss-braced wings.

Validated quasi-analytical mass estimation methods for innovative wing concepts.

Integrated assessment of mass, aerodynamics and performance for aircraft-level trades.

Experience in ATI/IUK funded projects, Airbus-led programmes, and academic collaborations.