Coordinatore | TECHNISCHE UNIVERSITAT BRAUNSCHWEIG
Organization address
address: POCKELSSTRASSE 14 contact info |
Nazionalità Coordinatore | Germany [DE] |
Totale costo | 429˙999 € |
EC contributo | 321˙599 € |
Programma | FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives |
Code Call | SP1-JTI-CS-2010-01 |
Funding Scheme | JTI-CS |
Anno di inizio | 2011 |
Periodo (anno-mese-giorno) | 2011-04-01 - 2014-06-30 |
# | ||||
---|---|---|---|---|
1 |
TECHNISCHE UNIVERSITAT BRAUNSCHWEIG
Organization address
address: POCKELSSTRASSE 14 contact info |
DE (BRAUNSCHWEIG) | coordinator | 119˙099.00 |
2 |
TECHNISCHE UNIVERSITAET DRESDEN
Organization address
address: HELMHOLTZSTRASSE 10 contact info |
DE (DRESDEN) | participant | 202˙500.00 |
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
'This proposal covers all actions from the university side required in the call JTI-CS-2010-1-SFWA-01-020 for the development and testing of two designs of an integration of active flow control concepts on a trailing edge of high lift devices, namely: • the design, including an optimization of the structure • the manufacturing of coupon specimens and a mock-up • the structural testing of the specimens The main technical challenge is the introduction of outlets in the highly loaded skin of the flap. Therefore, this is the main subject of the project, which leads beyond the state of the art.
For this purpose two universities are cooperating and rely on the work of EADS-IW as a partner within the Clean Sky consortium, making sure that new ideas on the integration of active flow control devices into the flap structure are investigated, and on the other hand that industrial manufacturing standards and certification rules are followed.
The DoW contains all work specified in the previously evaluated proposal but without the EADS-IW work share'
Although the jet engine provides the thrust for flight, lift is the job of the wings thanks to their aerodynamic shape. Active flow control (AFC) is the next rung on the wing's evolutionary ladder.
"Design, Manufacturing, Qualification and Assembly of an Improved NLF Wing Leading Edge and Upper Cover Flight Test Article"
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