Community Research and Development Information Service - CORDIS

Search projects and results

Results 1 - 10 of 1433
12 3 4 5 6 7 8 9 10 > >| 
Foldable, Adaptable, Steerable, Textile Wing Structure for Delivery of Capital Loads
ID: 30778
Start date: 2006-12-01, End date: 2010-06-30
FASTWing CL is to developing a navigated parafoil system for carrying loads of up to 6 tons. FASTWing CL is the successor of the FP5 programme. FASTWing which was completed successfully in June 2005. The latter has developed a prototype demonstrator capable to fly autonomous ...
Programme: FP6-AEROSPACE
Record Number: 81460
Last updated on: 2014-08-11
Study on High Altitude Aircrafts and Airships (HAAS), deployed for specific aeronautical and space applications
ID: 516081
Start date: 2005-03-01, End date: 2006-08-31
The proposed "USE HAAS" study objectives aim to examine prospective aeronautical research agenda in HAAS that European deployment of High Altitude Aircraft (HAIRCRAFT) or High Altitude Airship (HAIRSHIP) implies.Especially the main objectives of the pro ject are to develop a E...
Programme: FP6-AEROSPACE
Record Number: 75776
Last updated on: 2007-06-11
Flight reynolds number testing (1)
ID: 516118
Start date: 2005-02-01, End date: 2008-07-31
Conventional wind tunnels face physical limits matching Reynolds and Mach number ranges. Cryogenic wind tunnels, operating at temperatures as low as -163°C and with variable pressures, allow a realistic simulation of flight Reynolds and Mach numbers hence allowing a highly acc...
Programme: FP6-AEROSPACE
Record Number: 84785
Last updated on: 2009-09-27
Don Q Air
ID: 44666
Start date: 2007-01-01, End date: 2010-06-30
European RTD convergence is one of the most of the FP. Participation of SME especially from Eastern European as well as Candidate countries is far from being satisfactory. In response to this, Don Q Air intends to increase awareness of Polish, Romanian, and Turkish aeronautic ...
Programme: FP6-AEROSPACE
Record Number: 84161
Last updated on: 2010-09-24
Exploitation of AnGular effects in Land surfacE observations from satellites (EAGLE)
ID: 502057
Start date: 2004-02-01, End date: 2007-07-31
Remote sensing approaches using wide field of view scanners such as the AVHRR have often obviated the angular dependence of reflected and emitted radiation. Therefore the accuracy of the geophysical products derived does not meet the requested requirements for user communities...
Programme: FP6-AEROSPACE
Record Number: 72793
Last updated on: 2010-10-22
Supersonic transition control
[PROJECT] SUPERTRAC - Supersonic transition control
ID: 516100
Start date: 2005-01-01, End date: 2007-12-31
Skin friction drag on an aircraft wing has a significant impact on specific fuel consumption, pollution and noise emission. The objective of the SUPERTRAC project is to explore the possibilities of viscous drag reduction on supersonic aircraft wings by del aying TRAnsition. Th...
Programme: FP6-AEROSPACE
Record Number: 78734
Last updated on: 2007-06-11
Turbulence and Transition Modelling for Special Turbomachinery Applications
ID: 30939
Start date: 2006-10-01, End date: 2010-03-31
The TATMo project addresses the top level objectives outlined in the aeronautics research work programme, namely, improving the environmental impact with regards to emissions by improving the SFC and thus contributing to the reduction of CO2 emissions by 50% in the long term. ...
Programme: FP6-AEROSPACE
Record Number: 79964
Last updated on: 2012-03-08
Simulating aircraft stability and control characteristics for use in conceptual design
ID: 30838
Start date: 2006-11-01, End date: 2010-07-31
Present trends in aircraft design towards augmented-stability and expanded flight envelopes call for an accurate description of the non-linear flight-dynamic behaviour of the aircraft in order to properly design the Flight Control System (FCS). Hence th e need to increase the ...
Programme: FP6-AEROSPACE
Record Number: 81469
Last updated on: 2010-12-02
Ultra high temperature materials for turbines (ULTMAT)
ID: 502977
Start date: 2004-01-01, End date: 2008-06-30
The ULTMAT project aims at providing sound technological basis for the introduction of innovative materials, namely Mo- and Nb-base silicide multiphase alloys, which will allow a 100-150°C increase in airfoil material operating temperature in air-/rotorcraft engines and in aer...
Programme: FP6-AEROSPACE
Record Number: 72788
Last updated on: 2012-03-08
Long-Term Advanced Propulsion Concepts and Technologies
ID: 12282
Start date: 2005-04-15, End date: 2008-04-14
The objective is to identify and assess critical propulsion technologies required to reduce long-distance flights, e.g. from Brussels to Sydney, to less than 2 to 4 hours. Achieving this goal intrinsically requires a new flight regime for commercial transp ort with Mach number...
Programme: FP6-AEROSPACE
Record Number: 74769
Last updated on: 2011-06-02
12 3 4 5 6 7 8 9 10 > >| 
List retrieved on: 2018-05-20
Follow us on: RSS Facebook Twitter YouTube Managed by the EU Publications Office Top