Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
Cranfield University
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Output 0 of 0 in the submission
Article title
Optimum buckling design of composite stiffened panels using ant colony algorithm
Type
D - Journal article
Title of journal
Composite Structures
Article number
-
Volume number
92
Issue number
3
First page of article
712
ISSN of journal
0263-8223
Year of publication
2010
URL
-
Number of additional authors
3
Additional information
An output from research project funded by EPSRC/Airbus. A new optimization method was proposed and applied to a composite stiffened panel for maximum buckling capability. The optimization was subject to practical design rules employed in the aircraft A400M, based on real experience working within Airbus. The research has been evaluated by Airbus and will feed in to further development of the wing design optimization method. Contact: Benjamin John Phillip, A350 Program manager, Airbus, email address: BENJAMIN.PHILLIPS@airbus.com.
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
-
