Output details
15 - General Engineering
Queen Mary University of London
Article title
The fundamental solution of Mindlin plates resting on an elastic foundation in the Laplace domain and its applications
Type
D - Journal article
Title of journal
INT J SOLIDS STRUCT
Article number
-
Volume number
45
Issue number
3-4
First page of article
1032
ISSN of journal
0020-7683
Year of publication
2008
URL
-
Number of additional authors
0
Additional information
The cutting process for thin wall structures and the repair of components in aircraft structures such as stiffened wing skin and fuselage, requires thorough understanding of the dynamic response and stress distribution under impact forces including for example, moving cutting forces and bird-strike etc. The research study has led to the development of computational tools now widely used by Airbus UK to evaluate distortion of components in the fuselage and wing-box caused by residual stresses in billet. The paper led to three further industrial contracts with Airbus UK.
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
-
