Engine condition monitoring on small single engine turboprop
Improving the port selection process during military deployments
The use of FEA and semi-empirical equations for weight estimation of a passenger aircraft
Analysis of longitudinal dynamic stability of tandem wing aircraft
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations
Optimal energy management for hybrid-electric aircraft
Aerodynamic design of an electronics pod to maximise its carriage envelope on a fast-jet aircraft
A new simplified fluid dynamic model for digital twins of electrohydraulic servovalves
Modified vector field and nonlinear guidance law for low-cost UAV path following
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
Safety performance functions to predict separation minima infringements in en-route airspace