Abstract
A method for an assessment of the edge effect in curved laminates under four-point bend test is presented. The methodology uses ABAQUS FE analysis and the results are compared to the test results. FE analysis suggests that increase in strength from curved laminated with free edges to equivalent infinitely wide laminates can be as significant as 60%-120%. A way of reducing the edge effect by applying a thick layer of resin to the free edges is investigated using the developed methodology and compared against test results. Up to 19% increase in strength of curved elements with edge treatment has been confirmed in tests. Detailed FE analysis suggests that even greater edge effect mitigation, and therefore further increase in element strength, can be achieved if the contrast between the properties of the inter-laminar material and the resin used in edge treatment becomes smaller.
Original language | English |
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Title of host publication | Proceedings of the 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference |
Publisher | American Institute of Aeronautics and Astronautics Inc. |
ISBN (Print) | 9781624103421 |
DOIs | |
Publication status | Published - 2015 |
Event | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 - Kissimmee, USA United States Duration: 5 Jan 2015 → 9 Jan 2015 |
Conference
Conference | 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 |
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Country/Territory | USA United States |
City | Kissimmee |
Period | 5/01/15 → 9/01/15 |