Search for European Projects

5 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 ...
Read Project

 41

 FINISHED 

Design And Manufacture of Krueger Flaps (DEAMAK)

Start date: Oct 19, 2010, End date: Nov 18, 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 ...
Read Project

 1

 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 ...
Read Project

 21

 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 ...
Read Project

 3

 FINISHED 

AIRCRAFT INTEGRATED STRUCTURAL HEALTH ASSESSMENT II (AISHA II)

Start date: May 1, 2008, End date: Oct 31, 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 ...
Read Project

 14