Output details
15 - General Engineering
University of Glasgow
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Output 0 of 0 in the submission
Article title
Damage tolerance of fully orthotropic laminates in compression
Type
D - Journal article
Title of journal
Composites Science and Technology
Article number
-
Volume number
72
Issue number
10
First page of article
1083
ISSN of journal
0266-3538
Year of publication
2012
URL
-
Number of additional authors
2
Additional information
This research led to an important change in industrial practice; the move towards non-symmetric laminate designs for use in future aircraft structures (Contact: Thomas Kruse, Fuselage and Generic Structure Design Research, Thomas.Kruse@Airbus.com). The article demonstrates that anti-symmetric laminate designs provide the highest damage tolerance with respect to delamination buckling, and that the best symmetric and non-symmetric laminate designs offer comparable damage tolerance. The research was the result of collaboration with the University of Bath (Contact: R.Butler@Bath.ac.uk).
Interdisciplinary
-
Cross-referral requested
-
Research group
B - Infrastructure & Environment
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-