Online pre-print publication by UoL academics on the EU FP7 MAAT project • Smith T., Bingham C., Stewart P., Allarton R. and Stewart J., “Energy Harvesting and Power Network Architectures for the MAAT High Altitude Cruiser-Feeder Airship Concept”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Published online before print […]
EU FP7 Transport
Energy Harvesting and Power Network Architectures for the MAAT High Altitude Cruiser-Feeder Airship Concept
Online pre-print publication by UoL academics on the EU FP7 MAAT project • Smith T., Bingham C., Stewart P., Allarton R. and Stewart J., “Energy Harvesting and Power Network Architectures for the MAAT High Altitude Cruiser-Feeder Airship Concept”, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Published online before print […]
EU FP7 ACHEON Project CFD animations on YouTube
Two CFD animations about the ACHEON propulsion concept presented on 11 January 2013 during the ACHEON public event entitled – ACHEON Idee in azione – Un progetto aereonautico e le sue ricadute tecnologiche. The event tool place in Reggio Emilia, at Università degli Studi di Modena Reggio Emilia – DISMI ,Campus San Lazzaro, Pad Buccola. […]
ACHEON Aerial Coanda High Efficiency Orienting-jet Nozzle Kick-off Meeting report
Grant Agreement No. 309041 ACHEON Aerial Coanda High Efficiency Orienting-jet Nozzle 10-11 January 2013 www.acheon.eu Project Start Date: December 1st 2012 End Date: June 30th 2014 Co-ordinator: Università degli Studi Modena e Reggio Emilia (UniMoRe) ACHEON Kick-off Meeting Agenda Day 1 [Università degli Studi di Modena and Reggio Emilia, Dipartimento di Scienze e Metodi dell’Ingegneria, […]
EU FP7 ACHEON thrust vectoring project kick off meeting in Reggio Emilia
Today we are conducting briefings for the press and the European Commission on the ACHEON @acheonproject in the School of Engineering at the University of Reggio Emilia in Italy. ACHEON project explores the feasibility of a novel propulsive system for aircraft which is expected overcome the main limitations of traditional systems related to commonly […]