Project acronym |
Full title |
Application field |
Type |
3AS |
Active Aeroelastic Aircraft Structures |
Smart aeroelastic structural response |
FP5/ FP6 |
Prognostics and Health and Usage Monitoring |
Design of embedded computer hardware and software |
FP7 |
|
ANNA |
New materials for aircraft structure |
Novel composite structures |
National |
APART |
Advanced Powerplant and Aerodynamics Research Technology |
Civil Wing Technology |
UK National |
Aircraft Reliability Through Intelligent Materials Application |
Structural health monitoring |
FP6 |
|
Aerodynamic Validation of Emission Reducing Technologies |
Flow Control High-Lift & High Speed |
FP6 |
|
Advanced Wing And High-Lift Design |
High-lift devices for a next-generation wing on a regional aircraft context |
CS JTI-SFWA |
|
Aircraft Wing with Advanced Technology Operation |
Innovative wing and high-lift design means |
FP5 |
|
BUFET’N Co |
Boucle Fermée appliquee au tremblement 3D démonstration du contrôle |
Flow/buffet control |
ONERA internal project |
CS-JTI-SFWA-FloCoSys |
Clean Sky- Joint Technology Initiative-Smart Fixed Wing Aircraft- Efficient Flow Control Systems |
Flow control on flap |
FP7 |
Design And Manufacture of Krueger Flaps |
Design and manufacture of Krueger flaps |
CS-JTI-SFWA |
|
Design, Simulation and Flight Reynolds-Number Testing for Advanced High-Lift Solutions |
Aerodynamics for high-lift |
FP7 |
|
Development and Test of Fluidic Actuators for Active Flow Control |
Fluidic Acuator Design |
FP7 |
|
European High-Lift Programme I and II |
High-Lift design capabilties |
FP5/6 |
|
EXTream ICing Environements |
Icing |
FP7 |
|
Integration of technologies in support of a passenger end environmentally friendly helicopter |
Smart structures on helicopters |
FP6 |
|
HIGHER-LE |
High Lift Enhanced Research – Leading Edge |
HLFC |
National |
IMS & CPS |
Material Synergies & Composite Processing Strategies |
Carbon Fibre Reinforced Polymer (CFRC) |
FP7 |
Novel passenger aircraft configurations |
Novel concepts of aircraft design |
FP6 |
|
More Open Electrical Technologies |
Electrical Systems |
FP6 |
|
Optimisation for low Environmental Noise impact AIRcraft |
Low noise high-lift solutions |
FP7 |
|
Smart High Lift Devices for Next Generation Wings |
Testing of morphing structures for high-lift devices |
FP7 |
|
Smart Intelligent Aircraft Structures |
Morphing structures, integrated sensing structures, self-healing structures |
FP7 |
|
SAWoF |
Smart Active Wing of the Future |
Civil Wing Technology |
UK National |
SCAlable and ReconfigurabLe elEctronics plaTforms and Tools |
Design of embedded computer hardware and software |
FP7 |
|
CS-JTI-SFWA |
SFWA-ITD Smart Fixed Wing Aircraft Integrated Technology Demonstrator |
Flow & Loads Control, NLF |
FP7 |
SILENCER |
Significantly lower community exposure to aircraft noise |
Low noise aircraft design |
FP5 |
SimOD |
Aircraft Simulation at off-design Conditions |
Civil wing Design |
UK National |
SysTAvio |
System- und Avionik-Technologien der nächsten Generation |
OAD/Systems |
National |
Testing for Laminar Flow on New Aircraft |
Laminar flow |
FP6 |
|
Technologies to IMProve Airframe Noise |
Low noise design and treatments |
FP6 |
|
VER²SUS |
Verifikation und Validierung eines vereinfachten Absaugsystems |
HLFC verification and validation of a simplified suction system in a large scale wind tunnel test |
National: DLR project embedded in HIGHER:LE compound project |
HIGHER_LE |
Hight Lift Enhanced Research - Leading Edge |
HLFC: experimental demonstration of simplified suction concept, verification and validation of design methods (same as written at HIGHER) | National |
Application of Hybrid Laminar Flow Technology on Transport Aircraft | HLFC: concept of simplified suction developed | FP4 | |
MDX, HYLDA, LATEC |
Hybrid Laminar Flow Demonstration on Aircraft |
Feasibility of HLFC for transport aircraft proven |