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5 projets européens trouvés

Recherche sur 125080 projets européens

 TERMINÉ 

HiLamBiz

Date du début: 1 août 2013, Date de fin: 31 déc. 2015,

The proposal covers the preparation and performance of a wind tunnel test using an innovative Bizjet with natural laminar flow wings, RC-controlled HTP and nacelles. Model design, manufacturing and instrumentation will be supported for achieving a high quality model for a test in cryogenic environment. The tunnel will be instrumented for performance tests on a z-sting mounted full model acquiring ...
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 1

 TERMINÉ 

NLF Wing High Speed Performance Test (NLF-WingHiPer)

Date du début: 1 juil. 2014, Date de fin: 31 mars 2015,

The primary innovative approach and the major aim of the investigations being covered here is in the first instance to perform reliable and high quality procedures for laminar wing testing under and near flight conditions at high Reynolds numbers in ETW. Beside confirming a number of already mature and successfully applied measuring techniques, these investigations will allow to validate a new eva ...
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 1

 TERMINÉ 

European Strategic Wind Tunnels Improved Research Potential (ESWIRP)

Date du début: 1 oct. 2009, Date de fin: 30 sept. 2014,

...nels in Europe both in terms of productivity and quality. The concerned wind tunnels are ONERA S1MA Modane, DNW-LLF and ETW. The main ideas leading to the proposal have been (i) the identification at European level by the aeronautical community (ACARE) of the strategic wind tunnels for Europe needed to maintain and enhance the leadership of European aerospace industry and science,(ii) the EREA rec ...
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 3

 TERMINÉ 
...is planned for a period of 4 years and a budget of 7.6 Mio. Euro. The consortium consists of 6 industry partner, 7 research establishments, 3 universities, 2 small and medium-sized enterprise and the European Transonic Wind tunnel (ETW). Existing and validated high-fidelity numerical tools are composed to an efficient High-Lift design and optimization process chain in WP1. The strategies and too ...
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 21

 TERMINÉ 

Transonic High Reynolds Number Testing of a Large Laminar Wing Half Model (HiReLF)

Date du début: 25 juin 2012, Date de fin: 24 oct. 2012,

...minar Flow model refer to a key technology stream within the SFWA programme contributing to achieving the technology readiness level 6, thus supporting the realization of the Vision 2020 goals of the European Union.
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