Monner, Hans Peter und Riemenschneider, Johannes (2010) BACKGROUND AND RECENT RESULTS OF THE EUROPEAN PROJECT ‘SMART HIGH LIFT DEVICES FOR NEXT GENERATION WINGS’ (SADE). EASN Workshop on Aerostructures 2010, 2010-10-07 - 2010-10-08, Paris, Frankreich.
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Kurzfassung
Recent aerodynamic concepts for significant reduction of drag call for laminarization which requires slim high-aspect-ratio wings and increased surface quality. As consequence of these demands state-of-the-art high lift systems prove not to be feasible any more. Thus, the European project “Smart High Lift Devices for Next Generation Wings” (SADE), which started in May 2008 and has a duration of 4 years, brings together an interdisciplinary research team comprising reputable re-search institutes and universities, OEMs and SMEs to develop suitable morphing high lift devices: The seamless 'smart leading edge device' is an indispensable enabler for laminar wings and offers a great benefit for reduction of acoustic emissions, the 'smart single slotted flap' with active camber capability permits a further increased lift. Thanks to their ability to adapt the wing's shape, both devices also offer aerodynamic benefits for cruise flight. The technological realization and optimization of these concepts towards the special requirements of full scale systems is the main objective within SADE. This requires a detailed study of the aeroelastic condition the structural system has been optimized for. Hence, a realistic full scale section of a morphing wing will be manufactured and tested in the TsAGI T101 wind tunnel for an investigation of these effects. An overview of the project’s objectives, its structure and first results will be given within this paper
elib-URL des Eintrags: | https://elib.dlr.de/70487/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||
Titel: | BACKGROUND AND RECENT RESULTS OF THE EUROPEAN PROJECT ‘SMART HIGH LIFT DEVICES FOR NEXT GENERATION WINGS’ (SADE) | ||||||||||||
Autoren: |
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Datum: | Oktober 2010 | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
Stichwörter: | morphing; high lift; laminarization; smart structures; leading edge; trailing edge | ||||||||||||
Veranstaltungstitel: | EASN Workshop on Aerostructures 2010 | ||||||||||||
Veranstaltungsort: | Paris, Frankreich | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsbeginn: | 7 Oktober 2010 | ||||||||||||
Veranstaltungsende: | 8 Oktober 2010 | ||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||
HGF - Programmthema: | L VU - Luftverkehr und Umwelt (alt) | ||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||
DLR - Forschungsgebiet: | L VU - Luftverkehr und Umwelt | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Leiser Luftverkehr (alt) | ||||||||||||
Standort: | Braunschweig | ||||||||||||
Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Adaptronik | ||||||||||||
Hinterlegt von: | Böhringer-Thelen, Isolde | ||||||||||||
Hinterlegt am: | 21 Jul 2011 08:06 | ||||||||||||
Letzte Änderung: | 24 Apr 2024 19:35 |
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