Search for European Projects

8 European Projects Found

Searched on 125080 European Projects

 FINISHED 

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

Start date: Jun 1, 2013, End date: May 31, 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

 FINISHED 

Solar system plasma Turbulence: Observations, inteRmittency and Multifractals (STORM)

Start date: Jan 1, 2013, End date: Dec 31, 2015,

In this project we investigate solar system plasma turbulence from in-situ data gathered by automated platforms launched by the European Space Agency (ESA) and NASA. We investigate how the features of turbulence and intermittency vary with the solar activity and estimate the corresponding impact. We use electromagnetic field and plasma data provided by a core of three ESA spacecraft, Ulysses, Ve ...
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 9

 FINISHED 

Experimental TRansonic Investigations On Laminar flow and Load Alleviation (ETRIOLLA)

Start date: Jan 1, 2013, End date: Dec 31, 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

 FINISHED 

Industrialisation of High-Order Methods – A Top-Down Approach (IDIHOM)

Start date: Oct 1, 2010, End date: Mar 31, 2014,

"The proposed IDIHOM project is motivated by the increasing demand of the European aerospace industries to advance their CFD-aided design procedure and analysis by using accurate and fast numerical methods, so-called high-order methods. They will be assessed and improved in a top-down approach by utilising industrially relevant complex test cases, so-called application challenges in the general ar ...
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 21

 FINISHED 

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

Start date: Mar 1, 2009, End date: Jun 30, 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

 FINISHED 

Smart High Lift Devices for Next Generation Wings (SADE)

Start date: May 1, 2008, End date: Oct 31, 2012,

"All aerodynamic concepts for significant reduction of drag such as laminarisation require slim high-aspect-ratio wings. However, state-of-the-art high lift systems will suffer from the reduced construction space and do not cope with the required surface quality. Thus, SADE (Smart High Lift Devices for Next Generation Wings) develops suitable 'morphing' high lift devices: The seamless 'smart leadi ...
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 13

 FINISHED 

Advanced Wing And High-Lift Design (AWAHL)

Start date: Dec 1, 2010, End date: Jun 30, 2012,

"AWAHL will design a wing with its high-lift system for an advanced regional turbo-fan aircraft with optimal performance and efficiency. The wing will be designed with respect to the aerodynamic performance and constraints using in-house tools for CFD calculations and shape optimization. The design is carried out including optimization of the position of the pylon/nacelle. The aerodynamically opti ...
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 3

 FINISHED 

Assessment of LOw NOise COnfigurations (ALONOCO)

Start date: Jan 1, 2010, End date: Jun 30, 2011,

"ALONOCO will investigate the aerodynamic wing efficiency and the emitted noise from four different low-noise high-lift concepts of a regional aircraft. The concepts will be compared to a baseline configuration and ranked for down-selection. The analysis will be based on numerical simulations with high fidelity tools. The aerodynamic calculations will be based on steady and unsteady RANS, hybrid R ...
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 2