9 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
Experimental TRansonic Investigations On Laminar flow and Load Alleviation (ETRIOLLA)
Date du début: 1 janv. 2013, Date de fin: 31 déc. 2015,
"The proposal tackles the CfP JTI-CS-2012-1-GRA-02-019. Within the project a Wind-Tunnel-Model is designed, built and tested that is capable of being tested with two main purposes:- access the extend of laminarity on the wing- evaluate the performance of LC&A system in the trailing edge of the wingIn order to do this the project tackles different points:- a model design is performed that creates a ...
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4
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TERMINÉ
Experimental Acoustic Subsonic wind tunnel Investigation of the advanced geared turbofan Regional aircraft integrating HLD innovative low-noise design (EASIER)
Date du début: 1 juin 2014, Date de fin: 31 oct. 2015,
...nce for this project:- IBK is a small company coordinating the project and performing design work in the project. IBK is also leading the consortium building the WT in the previous project ESICAPIA.- REVOIND is a small italian company specialised in manufacturing complex parts. Revoind´s main task in this project is to manufacture the model.- University of Rome, Prof. Camussi, bringt acoustic know ...
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4
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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,
...l test under low-speed conditions.The consoritum set up for this proposal therefore consists of companies specialisied in the three doamins. IBK will coordinate the consortium and perform the design. Revoind Industriale is performing the manufacturing, RUAG as third partner will focus on the engine development.The proposal tackling these different tasks will introduce a number of highly innovative ...
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4
Participants partenaires
TERMINÉ
WindTunnel Tests on an Innovative regional A/C for Noise assessment (WITTINESS)
Date du début: 1 oct. 2014, Date de fin: 30 sept. 2015,
... build up as follows:- IBK is a small company coordinating the project and performing design work in the project. IBK is also leading the consortium building the WT in the previous project ESICAPIA.- REVOIND is a small italian company specialised in manufacturing complex parts. Revoind´s main task in this project is to manufacture the model.- University of Rome, Prof. Camussi, bringt acoustic know ...
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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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