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 - Eight-Foot High Speed Tunnel - Document - PDFSEARCH.IO

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Date: 2014-12-12 04:55:59 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 the Add to Reading List Source URL: www.cleansky.eu Download Document from Source Website File Size: 347,15 KB Share Document on Facebook

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