3 projets européens trouvés
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TERMINÉ
invEstigation of a contRA rotating open rotor engine Configuration trough wind tunneL Experiments (ERACLE)
Date du début: 1 janv. 2016, Date de fin: 30 avr. 2017,
In the framework of the airframe (AIR) ITD work package, as required by the JTI-CS2-2014-CFP01-AIR-01-04, the ERACLE project is aimed to assess the impact on tonal and broadband noise of the “core flow into propeller” architecture versus the conventional CROR architecture through wind tunnel test in low speed conditions. Going in detail of technical aspects, the ERACLE consortium will support the ...
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3
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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
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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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