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 TERMINÉ 
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 

Design And Manufacture of Krueger Flaps (DEAMAK)

Date du début: 19 oct. 2010, Date de fin: 18 nov. 2016,

... Such accumulations and erosions, resulting in wing surface discontinuities, could significantly increase friction drag by causing loss of laminar flow in the affected areas.In the frame of DEAMAK, ASCO Industries N.V., a Belgian company involved in the development of the high-lift devices on all recent major aircraft programs (A380, A400M, Boeing 787, A350XWB, Bombardier CSeries), will design and ...
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 1

 TERMINÉ 

Advanced Intelligent Machine Adaptive Control System (AIMACS)

Date du début: 1 août 2010, Date de fin: 31 juil. 2013,

"Current machining technologies and practices have many inefficiencies. Numerous unpredictable machining variables often cause overload and unstable conditions and catastrophic damage to the machine tool system. In addition, this results in frequent disruptions in production that can often be excessive, leading to considerable losses in productivity, capital and energy resources. In an effort to p ...
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 10

 TERMINÉ 
"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

 TERMINÉ 

Advanced Wing And High-Lift Design (AWAHL)

Date du début: 1 déc. 2010, Date de fin: 30 juin 2012,

...ximum budget is estimated to 450,000 €. The consortium consists of three partners, the Swedish research organisation FOI being the coordinator, the Italian university POLIMI and the Belgian company ASCO. All three partners are highly capable, well established and active in national and European collaborative programs related to aerodynamic, aero-elastic and high-lift design and simulations."
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 3

 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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 14