Stiffness corrections for overlaps and gaps in steered composite panel optimization
Stiffness corrections for overlaps and gaps in steered composite panel optimization
In this paper, a method is introduced that predicts the influence of gaps and overlaps introduced by fiber steering on the stiffness and strength of composite laminates. This method is based on the incorporation of a “density functional” which translates the effect of discrete gaps and laps into a continuous correction of the reduced stiffness matrix. It also includes a function to incorporate a fiber placement manufacturing strategy. Test configurations used to test the validity of the density functional approach show results consistent with the expected gap/overlap distributions, and also demonstrate the robustness of the manufacturing strategy function. The method is to be included in the TopSteer optimization code1 to study the influence of gaps and overlaps on optimization results
American Institute of Aeronautics and Astronautics
van Tooren, Michel J. L.
1be91e33-ee5a-47c2-891d-4dff1f454c27
Lucas, David A.
9ca8afbc-75ab-4d39-b640-fd6783fed275
Elham, A.
676043c6-547a-4081-8521-1567885ad41a
13 January 2017
van Tooren, Michel J. L.
1be91e33-ee5a-47c2-891d-4dff1f454c27
Lucas, David A.
9ca8afbc-75ab-4d39-b640-fd6783fed275
Elham, A.
676043c6-547a-4081-8521-1567885ad41a
van Tooren, Michel J. L., Lucas, David A. and Elham, A.
(2017)
Stiffness corrections for overlaps and gaps in steered composite panel optimization.
In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017.
American Institute of Aeronautics and Astronautics..
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Abstract
In this paper, a method is introduced that predicts the influence of gaps and overlaps introduced by fiber steering on the stiffness and strength of composite laminates. This method is based on the incorporation of a “density functional” which translates the effect of discrete gaps and laps into a continuous correction of the reduced stiffness matrix. It also includes a function to incorporate a fiber placement manufacturing strategy. Test configurations used to test the validity of the density functional approach show results consistent with the expected gap/overlap distributions, and also demonstrate the robustness of the manufacturing strategy function. The method is to be included in the TopSteer optimization code1 to study the influence of gaps and overlaps on optimization results
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Published date: 13 January 2017
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© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Venue - Dates:
AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, , Grapevine, United States, 2017-01-09 - 2017-01-13
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Local EPrints ID: 470909
URI: http://eprints.soton.ac.uk/id/eprint/470909
PURE UUID: b72af3be-5712-4f5b-b337-58f70b6e3d33
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Date deposited: 20 Oct 2022 16:52
Last modified: 11 Mar 2024 18:02
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Contributors
Author:
Michel J. L. van Tooren
Author:
David A. Lucas
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