On composite laminates with extensional anisotropy

York, C.B. (2008) On composite laminates with extensional anisotropy. In: 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Schaumburg, IL, USA, 7-10 Apr 2008, (doi:10.2514/6.2008-1752)

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Publisher's URL: http://dx.doi.org/10.2514/6.2008-1752

Abstract

The definite list of extensionally (membrane) anisotropic composite laminates with up to 21 plies is presented. The listings comprise of individual stacking sequences, which are characterized in terms of angle- and cross-ply sub-sequence relationships as well as the blend-ratio of unbalanced angle-plies. Dimensionless parameters, including lamination parameters, are provided, from which the extensional and bending stiffness terms are readily calculated and an assessment of the bending stiffness efficiency made for angle- and cross-ply sub-sequences. Comparisons are made between the structural response of extensionally-anisotropic laminates and laminates with both extensional- and bending-anisotropy; Initial- and post-buckling responses are considered at the panel level together with the static response of a complete wing-box structure.

Item Type:Conference Proceedings
Keywords:loads alleviation technology
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:York, Dr Christopher
Authors: York, C.B.
Subjects:T Technology > T Technology (General)
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences
University Centres > Glasgow Materials Research Initiative
Publisher:American Institute of Aeronautics and Astronautics
Copyright Holders:Copyright © 2008 The Author
First Published:First published in the Proceedings of the 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Publisher Policy:Reproduced with permission of the author

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