Assessment of Conceptual Hybrid-Electric Regional Aircraft with Boundary-Layer Ingestion Propeller

Development of a Software Architecture for a Reconfigurable Aircraft Design System

Aerodynamic Design Integration of Strut Braced Wings

Propeller Slipstream Effects on Longitudinal Static Stability: Effect of the Rethorst Correction at the Horizontal Stabilizer

Coupled hybrid electric aircraft design and strategic airline planning

A Conceptual aircraft design methodology for parallel hybrid-electric powertrains: Prediction of engine performance and electric component integration

Aerodynamic Design and Analysis of a Two Stage to Orbit Winged semi-Reusable Launching Vehicle

Positioning of the Ducted Fan Propulsive Stabiliser

Fuel Tank Integration for Hydrogen Airliners

Application of Power Balance Method to CFD

An Assessment of a Regional Turboprop Featuring Wingtip-Mounted Propellers: Design Integration Coupling Propeller-Wing Aerodynamics and Structural Wing Weight

Mission assessment for hybrid-electric single aisle aircraft

Structural Sizing Method for Propulsive Empennage System: Weight Estimation of Ducted Propeller Systems that Provide Longitudinal and Lateral Stability

Investigation of the benefits of a parallel-hybrid electric architecture in NOx,CO and H2O emissions in the LTO cycle for regional turboprop

Supporting MDO through dynamic workflow (re)generation

Drag reduction through a streamlined aerodynamic design process: Development and implementation of a methodology to accelerate the aerodynamic design process in the preliminary phase of car design