Engine condition monitoring on small single engine turboprop
The use of FEA and semi-empirical equations for weight estimation of a passenger aircraft
Development process for preliminary aircraft sizing methods with regard to new technologies
Editorial: Entangling the conceptual, disruptive, pragmatic, and relational
An innovative material for space-oriented structures and habitat design
Aerodynamic design of an electronics pod to maximise its carriage envelope on a fast-jet aircraft