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Horizon 2020 project information and now also report summaries are available on CORDIS. All H2020 projects can be downloaded from the EU Open Data Portal .

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ID: 278419
Start date: 2011-09-01, End date: 2013-10-31
"In the 1980s, many research work was performed, manly in the US, on new propulsion technology, at that time named “prop-fan”, that have the objective to reduce significantly the fuel consumption. WENEMOR has been developed in response to the requirements described in the Cle...
Programme: FP7-JTI
Record Number: 100688
Last updated on: 2015-03-10
Acoustic and thermal instrumentation, tests and modelling of engine surface coolers in representative aerodynamic conditions
ID: 255881
Start date: 2010-01-01, End date: 2013-02-28
The present proposal addresses the acoustic and thermal instrumentation, tests and modelling of engine surface coolers in representative aerodynamic conditions. In addition to aerodynamic tests already performed on surface coolers in a regional funded project, complementary t...
Programme: FP7-JTI
Record Number: 97987
Last updated on: 2017-05-29
Landing Gear Noise Attenuation
[PROJECT] NOISETTE - Landing Gear Noise Attenuation
ID: 271886
Start date: 2013-01-01, End date: 2014-01-31
"Within NOISETTE, Cenaero and VKI combine their respective expertise in computational fluid dynamics and acoustics in order to deliver a tailored solution for the aero-acoustic assessment and design of a low-noise configuration for a regional aircraft nose landing gear. The c...
Programme: FP7-JTI
Record Number: 106995
Last updated on: 2015-03-10
Multipurpose Aircraft Simulation Laboratory
ID: 255907
Start date: 2010-01-01, End date: 2012-08-31
The tendency of the past to build and test in aeronautics has clearly been overridden by a very extensive simulation activity for many reasons, one of these being the risk associated to safety-critical or safety-related systems. Simulation in hence strategic to develop and te...
Programme: FP7-JTI
Record Number: 98043
Last updated on: 2017-05-26
Advanced Turbofan-Equipped Aircraft Noise Model
ID: 255750
Start date: 2010-01-01, End date: 2012-08-31
The aim of this project is to adapt, improve validate and test a computer model for the simulation of aircraft noise. The project starts from a well-established basis of a multi-disciplinany computer model that includes flight mechanics, aerodynamics, gas turbine engine perfo...
Programme: FP7-JTI
Record Number: 98025
Last updated on: 2017-05-26
Leading Edge Box Design for Swept Flow Control Wing
ID: 255752
Start date: 2010-01-01, End date: 2012-09-30
The subject of the proposed project LEBox will be design of an integrated leading edge (L/E)-Box with pneumatic flow control devices for mid-scale wind tunnel testing on a suitable swept constant chord (2.5D) model. Dynamic vortex generator jets (VGJs) are chosen as the most ...
Programme: FP7-JTI
Record Number: 98026
Last updated on: 2017-05-26
Numerical Tool for Aerodynamic Optimization of Laminar Wings
ID: 255732
Start date: 2010-01-01, End date: 2011-04-30
The classical numerical approach used for Natural Laminar Flow (NLF) design relies on the experience of the engineers in finding pressure distributions that would improve the extent of laminar flow and could reasonably be approximated in an inverse design phase. Recent initia...
Programme: FP7-JTI
Record Number: 97985
Last updated on: 2017-05-29
Sustainable recycling of aircrafts composites
ID: 296546
Start date: 2011-12-01, End date: 2013-11-30
"The project aims at developing a sustainable, cost effective, purely physical approach to the recycling of thermosetting and thermoplastic carbon fibres reinforced composites typically obtained from the dismantling of End-of-Life Aircrafts. A preliminary investigation will b...
Programme: FP7-JTI
Record Number: 101279
Last updated on: 2015-03-10
Assessment of the interaction of a passive and an active load alleviation scheme
ID: 287020
Start date: 2011-07-01, End date: 2012-12-31
"In PALAST active and passive load alleviation techniques will be reviewed together. The passive measures require modification of the primary structure and thus influence the dynamic response of the wing. An active load alleviation scheme for an aircraft is based on its stati...
Programme: FP7-JTI
Record Number: 102329
Last updated on: 2015-03-10
NTN-SNR Proposal for Propellers Blades Bearings Design and Manufacturing
ID: 326023
Start date: 2013-02-04, End date: 2015-12-03
NTN-SNR is a major supplier for the propellers blade bearing. That is why NTN-SNR answers to this topic of call 12. The global strategy of the project is divided into 4 major tasks which constitute the work packages of the project (WP2 to WP5) and one work package is dedicate...
Programme: FP7-JTI
Record Number: 108810
Last updated on: 2015-10-23
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List retrieved on: 2018-03-22
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