6 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Design and Manufacturing of Baseline Low-Speed, Low-Sweep Wind Tunnel Model (EULOSAM)
Date du début: 1 juin 2013, Date de fin: 31 déc. 2016,
The EULOSAM project will deliver a large scale half-model to be tested in a pressurized low speed wind tunnel (WT). The model design will be performed under a previous CfP topic (JTI-CS-2010-3-SFWA-02-007), while Dassault Aviation will deliver a fuselage that has to be modified in order to fit the new laminar wing. The fuselage modifications must be designed in such a way that the fuselage can re ...
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4
Participants partenaires
TERMINÉ
TEst of Tilt-Rotor Air intakes (TETRA)
Date du début: 1 févr. 2014, Date de fin: 31 déc. 2016,
The project pertains to the wind tunnel testing of the engine air-intakes of a tilt-rotor aircraft. The testing activity aims to evaluate the effectiveness of the internal intake duct shape optimisation performed by GRC. Both the original and the optimised duct geometries will be tested in a purposely designed and manufactured nacelle model which includes the rotor hub and the external part of the ...
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2
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TERMINÉ
Gust Load Alleviation techniques assessment on wind tUnnel MOdel of advanced Regional aircraft (GLAMOUR)
Date du début: 1 févr. 2014, Date de fin: 30 sept. 2016,
The aim of Gust Load Alleviation techcniques assessment on wind tUnnel MOdel of advanced Regional aircraft (GLAMOUR) proposal is a technological optimisation and experimental validation through an aero-servo-elastic innovative WT model of gust load alleviation control systems for advanced Green Regional Aircraft. The expected benefits of such technologies are mainly the mitigation of gust load res ...
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5
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TERMINÉ
LOw Subsonic Investigationof a largecomplete Turboprop Aircraft (LOSITA)
Date du début: 1 oct. 2013, Date de fin: 30 sept. 2015,
The project tackles the design, manufacturing and testing of an advanced turob-prop 90-seat regional aircraft complete powered model. The model will be tested in a Wind-Tunnel with the aim of evaluation the performance of the high-.lift devices in different configurations.Major work-packages therefore are the design and manufacturing of the model, the design and manufacturing of a engine demonstra ...
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4
Participants partenaires
TERMINÉ
Experimental Subsonic Investigation of a Complete Aircraft Propulsion system Installation and Architecture power plant optimization (ESICAPIA)
Date du début: 1 juin 2013, Date de fin: 31 mai 2015,
The proposed project tackles a CfP from the JTI-GRA ITD. Is focuses on the experimental optimization of a regional aircraft configuration and a subsequent optimization of take-off/ landing configuration. The regional aircraft has a wing designed for natural laminar flow, fuselage-mounted engines and a T-tail. Open configurational questions that are addressed tackle wing-tip devices and their perfo ...
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5
Participants partenaires
TERMINÉ
DEsign and Manufacturing of a pitch-Oscillating System for gurney flap testing (DEMOS)
Date du début: 1 juin 2013, Date de fin: 31 mai 2015,
"The development of new innovative rotorcraft vehicles requires strong investments in the field of R&D adopting advanced numerical tools and innovative experimental methodologies.The dynamic stall phenomenon has been the subject of considerable interest in helicopter and aircraft manoeuvrability.Preliminary results showed that the Active Gurney flap can delay the dynamic stall phenomenon, but furt ...
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