Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
Cranfield University
Return to search
Output 0 of 0 in the submission
Article title
Aeroelastic dynamic response and control of an airfoil section with control surface nonlinearities
Type
D - Journal article
Title of journal
Journal of Sound and Vibration
Article number
-
Volume number
329
Issue number
22
First page of article
4756
ISSN of journal
0022-460X
Year of publication
2010
URL
-
Number of additional authors
2
Additional information
This paper resulted from an EC funded FP7 research project “Smart high lift devices for next generation wings (SADE)”, which involved 13 partners including EADS, Airbus, DLR, FOI and TsAGI. The morphing mechanism and modelling developed provide a practical and effective design to improve the aerodynamic performance of the whole wing, especially in take-off and landing. The research has led to evaluation at EADS/Airbus/DLR, assisting further development of morphing wing technology in the next EC framework CleanSky-2. Contact: Hans Peter Monner, Head of Adaptronics Dept, DLR, Germany, email: hans.monner@dlr.de.
Interdisciplinary
-
Cross-referral requested
-
Research group
F - Structures and Machine Systems
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
