Output details
14 - Civil and Construction Engineering
University of Leeds
Article title
Bilevel optimization of blended composite wing panels
Type
D - Journal article
Title of journal
Journal of Aircraft
Article number
-
Volume number
48
Issue number
1
First page of article
107
ISSN of journal
00218669
Year of publication
2011
URL
-
Number of additional authors
3
Additional information
The complexity of a mixed integer-discrete optimisation problem with an FE simulation in the loop (as found in the design of composite aircraft wings) means the system is not solvable by existing means. This paper presents a new method to reduce this complexity to a manageable level. This work has lead to the involvement in the EU project "Advanced lattice Structures for Composite Airframes" (AlaSCA, No. 265881, € 3,431,752) in partnership with EADS, Airbus, TU Delft amongst others.
Interdisciplinary
-
Cross-referral requested
-
Research group
None
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
