Propulsion system integration for aeropropulsive augmentation of a low-speed unmanned aerial vehicle
The Journal of Defense Modeling and Simulation: Applications, Methodology, Technology
Published online on March 12, 2026
Abstract
The Journal of Defense Modeling and Simulation, Ahead of Print.
A study on the integration of an Electric Ducted Fan (EDF) serving as the propulsion system with the aerodynamic field of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) operating at low Mach numbers is presented. The aim is to investigate the ...
A study on the integration of an Electric Ducted Fan (EDF) serving as the propulsion system with the aerodynamic field of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) operating at low Mach numbers is presented. The aim is to investigate the ...