5 projets européens trouvés
Recherche sur 125080 projets européens
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
Participants partenaires
TERMINÉ
Design And Manufacture of Krueger Flaps (DEAMAK)
Date du début: 19 oct. 2010, Date de fin: 18 nov. 2016,
"Natural Laminar Flow is one of the principal new wing technologies to be applied in the near future to reach the challenging fuel consumption and emission reduction objectives stipulated in ACARE’s Vision 2020. NLF airfoils are shaped in such a way to avoid laminar to turbulent flow transitions in cruise which creates increased viscous drag, hence larger fuel consumptions and more emissions.Krueg ...
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1
Participant partenaire
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
Participants partenaires
TERMINÉ
Advanced Wing And High-Lift Design (AWAHL)
Date du début: 1 déc. 2010, Date de fin: 30 juin 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
Participants partenaires
TERMINÉ
AIRCRAFT INTEGRATED STRUCTURAL HEALTH ASSESSMENT II (AISHA II)
Date du début: 1 mai 2008, Date de fin: 31 oct. 2011,
"The safe use of complex engineering structures such as aircrafts can only be guaranteed when efficient means of damage assessment are in place. Whereas the design of civil structures is nowadays based on a damage tolerance approach and time based inspection cycles, it is envisaged that the large cost associated with this approach can be drastically reduced by switching to a condition based mainte ...
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