Crashworthiness Design with Bending Optimization in the Hybrid Cellular Automata Framework: A Design Methodology for Aircraft Sub-Floor Structures

Hangar Parking Optimization with Path Planning Integration: A novel Approach to Minimize Movements via A* Adaptations and Neighborhood Search

Inlet Design for a Propulsive Fuselage Concept: Exploring and evaluating geometrical inlet features based on a numerical approach

Aircraft component health analysis for predictive maintenance: using a dilated convolutional autoencoder and KL divergence

Preliminary design methods for the thermal management of fuel cell powered aeroengines

Conceptual Design of Fuel Cell Commuter Aircraft: A study into the performance and viability of CS-23 category transport aircraft utilising hydrogen fuel cell propulsion

Crashworthiness Analysis of An Aircraft Subfloor Structure using Artificial Neural Networks

Weight Estimation of Gas Turbine Engines: Development of a Component-Based Preliminary Engine Design Tool

Design of Propulsion System for 9 PAX Electric Aircraft: Energy Storage and Transfer

Uncertainty modelling in remaining useful life estimations of aircraft engines

Analysis and optimization of thermoplastic fuselage struts under crashworthiness requirements

Techno-Economic feasibility analysis of Solid-Oxide Fuel Cell-Gas Turbine based hybrid propulsion system fueled by Hydrogen: How a Solid-Oxide Fuel Cell can impact the performance of the propulsion system and the economics of the aircraft

High capacity Continuous Descent Operations: A case study of Amsterdam airport Schiphol

Can Hail Impacts Trigger Delaminations?: A qualitative study to evaluate the consequences of hail ice impact on composite structures.

Design of a crash energy absorber for a composite aircraft fuselage using a combined analytical-numerical approach

Simulating order fulfillment for aircraft line replaceable unit strategy: A case study at KLM component services

Mission assessment for hybrid-electric single aisle aircraft

A coupled propulsion and thermal management system for hybrid electric aircraft design: A case study

Operational Gate Allocation Using a Sliding Time Window

Finding the climate optimal cruise altitude for a selection of aircraft types and mission combinations