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Control and Alleviation of Loads in Advanced Regional Turbo Fan Configurations

Ziel

A novel adaptive winglet concept will be developed to enable controlled cant angle orientation and twist throughout the flight envelope whilst also providing a passive gust loads alleviation capability. A CFD based aerodynamic design of the device applied on a baseline Turbo-Fan Aircraft configuration model will be undertaken, followed by a preliminary lay-out definition of the structure and actuation system required for the device. Detailed parametric studies will then be performed to investigate the performance of the device in terms of both drag and loads alleviation capabilities on its own, and also in combination with conventional control actuators, and both compared to the baseline configuration.

Aufforderung zur Vorschlagseinreichung

SP1-JTI-CS-2010-05
Andere Projekte für diesen Aufruf anzeigen

Koordinator

UNIVERSITY OF BRISTOL
EU-Beitrag
€ 111 663,00
Adresse
BEACON HOUSE QUEENS ROAD
BS8 1QU Bristol
Vereinigtes Königreich

Auf der Karte ansehen

Region
South West (England) Gloucestershire, Wiltshire and Bristol/Bath area Bristol, City of
Aktivitätstyp
Higher or Secondary Education Establishments
Kontakt Verwaltung
Julie Coombs (Mrs.)
Links
Gesamtkosten
Keine Daten

Beteiligte (3)