Development of a new conceptual design methodology for parallel hybrid aircraft
Towards a methodology for new technologies assessment in aircraft operating cost
New methodology for flight control system sizing and hinge moment estimation
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations
On-Board Systems Preliminary Sizing in an Overall Aircraft Design Environment (AIAA 2017-3065)
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft
Diesel engine application on AEW&C turboprop effectiveness-cost assessment
Preliminary design of a cabin escape system for a suborbital vehicle aimed at parabolic flights