A New Perspective on Battery-Electric Aviation, Part I: Reassessment of Achievable Range

Analysing the Role of the Propulsive System in the Global Civil Aviation Energy Optimisation Framework

Half a Tube&Wing: Function-to-Form Mapping Approach to Understanding Fixed-Wing Civil-Aeroplane Design Space

Fixed-Wing Aeroplane (Sub)System Design Method: From Abstract to Material Architectures

Preliminary Design and Optimization of a CubeSat Demonstrator for an Origami-inspired Deployable Structure

Aeroelastic Model for Design of Composite Propellers

Booster Fly-Back Analysis of Reusable Launch Systems

Swept Transition Experimental Platform (STEP)

Integrated Shape and Trajectory Optimisation of Hypersonic Waveriders

Gravity-Field Estimation of Asteroids

Aeroelastic Tailoring of a Strut-Braced Wing for a Medium Range Aircraft

High-Dimensional Bayesian Optimisation with Large-Scale Constraints - An Application to Aeroelastic Tailoring

Optimal Control for Distributed Aeroelastic Morphing Structure with Uncertainties and Imperfections

Incremental Nonlinear Dynamic Inversion control with Flight Envelope Protection for the Flying-V

Certification of Reinforcement Learning Applications for Air Transport Operations Based on Criticality and Autonomy

Optimization of Tollmien-Schlichting waves control: comparison between a deep reinforcement learning and particle swarm optimization approach

Parametric study of a switchable vortex generator for load alleviation in transonic conditions

Rapid Aerostructural Optimization of Wing-Propeller Systems

How Ready a Municipality is for Zero-Emission City Logistics? Development and Application of Maturity Model for Dutch Municipalities

Blade Element Theory Model for UAV Blade Damage Simulation