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Content archived on 2024-06-18

Control and Alleviation of Loads in Advanced Regional Turbo Fan Configurations

Objective

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.

Call for proposal

SP1-JTI-CS-2010-05
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Coordinator

UNIVERSITY OF BRISTOL
EU contribution
€ 111 663,00
Address
BEACON HOUSE QUEENS ROAD
BS8 1QU Bristol
United Kingdom

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Region
South West (England) Gloucestershire, Wiltshire and Bristol/Bath area Bristol, City of
Activity type
Higher or Secondary Education Establishments
Administrative Contact
Julie Coombs (Mrs.)
Links
Total cost
No data

Participants (3)