Output details
12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering
University of Northampton
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Article title
A dynamic stiffness element for free vibration analysis of composite beams and its application to aircraft wings
Type
D - Journal article
Title of journal
Computers & Structures
Article number
-
Volume number
86
Issue number
6
First page of article
573
ISSN of journal
00457949
Year of publication
2008
URL
-
Number of additional authors
2
Additional information
The powerful and elegant dynamic stiffness method is developed for composite beams exhibiting geometric and material coupling between bending and torsional motions. The theory developed paves the way for modal analysis of high aspect ratio composite wings and provides prospects for aeroelastic studies to achieve desirable objectives when designing a composite wing.
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
-
