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12 projets européens trouvés

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 TERMINÉ 

Increased Safety and robust certification for ditching of aircrafts and helicopters (SARAH)

Date du début: 1 oct. 2016, Date de fin: 30 sept. 2019,

SARAH is concerned with establishing novel holistic, simulation-based approaches to the analysis of aircraft ditching. It is build up from a consortium of experts from OEM industries, experienced suppliers of simulation technologies, established research institutions and representatives of the certification authorities. Results of SARAH are expected to support a performance-based regulation and ce ...
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 12

 TERMINÉ 

"""2nd Generation Active Wing“ – Active Flow- Loads & Noise control on next generation wing" (AFLONEXT)

Date du début: 1 juin 2013, Date de fin: 31 mai 2018,

AFLoNext is a four year EC L2 project with the objective of proving and maturing highly promising flow control technologies for novel aircraft configurations to achieve a quantum leap in improving aircraft’s performance and thus reducing the environmental footprint. The project consortium is composed by forty European partners from fifteen countries. The work has been broken down into seven work p ...
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 41

 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

 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

 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

 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

 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,

EASIER adresses the CfP JTI_CS_2013-2-GRA-05-008 and proposes a way to perform acoustic tests on a WT-model which was designed and manufactured in a previous CfP.The current project is proposed by a small consortium combining the necessary competence for this project:- IBK is a small company coordinating the project and performing design work in the project. IBK is also leading the consortium buil ...
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 4

 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,

WITTINESS adresses the acoustic measurement campaign of previously (in a different CfP) designed WT-model, equipped with engine-demonstrators. In order to tackle this project a consortium including a company experienced in design, structural mechanics and aerodynamics, a SME, a manufacturer and a university with a strong focus on acoustic measurements propose an approach to use the previously desi ...
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 4

 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

 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

 TERMINÉ 

Active Flow Control Technique on Trailing Edge Shroud for Improved High Lift Configurations (ATTESI)

Date du début: 1 juin 2011, Date de fin: 28 févr. 2014,

"The subject of the proposed project ATTESI is the design and evaluation of flow control techniques to improve the separation behavior on a drooped spoiler configuration.The proposed project comprehends numerical evaluation and optimization of the spoiler droop together with different flow control approaches applied upstream of the kink (the effect of the droop) and at the trailing edge of the spo ...
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 4

 TERMINÉ 

"Design, Simulation and Flight Reynolds Number Testing for Advanced High-Lift Solutions" (DESIREH)

Date du début: 1 mars 2009, Date de fin: 30 juin 2013,

"DeSiReH focus on both, the numerical design tools and the experimental measurement techniques for cryogenic conditions, with the objective to improve the industrial design process for laminar wings in terms of product quality, efficiency, and development cost reduction. The work focuses on the design of high lift devices. DeSiReH addresses the following quantified objectives which will make a sig ...
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 21