PT656 Gurney flap actuator and mechanism for a full scale helicopter rotor blade State of the art – Background Active Gurney Flap (AGF) system that is being developed in PT656 Program takes credit from the - Full-Scale Wind Tunnel - Document - PDFSEARCH.IO

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	PT656 Gurney flap actuator and mechanism for a full scale helicopter rotor blade State of the art – Background Active Gurney Flap (AGF) system that is being developed in PT656 Program takes credit from the Add to Reading List Document Date: 2014-12-12 04:55:59 Open Document File Size: 347,15 KB Share Result on Facebook Company MICROTECNICA SRL / Marco Gianfranceschi UTC Aerospace Systems / / Country Italy / / Currency EUR / / / Facility University of Bristol / IT UNIVERSITY OF BRISTOL UK POLITECNICO DI TORINO IT / / IndustryTerm active/passive anti-vibration systems / blade devices / / Organization Politecnico di Torino / University of Bristol / IT UNIVERSITY OF BRISTOL UK POLITECNICO DI TORINO IT / Sébastien Dubois sebastien.dubois@cleansky.eu Participating / / / Position representative / months Coordinator / Project Officer / / RadioStation 2013 Wind / / SocialTag Aviation Gurney flap Helicopter Wind tunnel VTOL aircraft Aerospace engineering Aircraft Helicopter rotor

PT656 Gurney flap actuator and mechanism for a full scale helicopter rotor blade State of the art – Background Active Gurney Flap (AGF) system that is being developed in PT656 Program takes credit from theAdd to Reading List