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Evolution of ply cr...
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Singh, Chandra VeerDepartment of Aerospace Engineering, Texas A&M University
(författare)
Evolution of ply cracks in multidirectional composite laminates
- Artikel/kapitelEngelska2010
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Elsevier BV,2010
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printrdacarrier
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LIBRIS-ID:oai:DiVA.org:ltu-10146
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https://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-10146URI
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https://doi.org/10.1016/j.ijsolstr.2010.01.016DOI
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Språk:engelska
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Sammanfattning på:engelska
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Ämneskategori:ref swepub-contenttype
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Ämneskategori:art swepub-publicationtype
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Upprättat; 2010; 20130124 (andbra)
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This paper treats evolution of ply cracks in multidirectional composite laminates subjected to a quasi-static tensile load in the longitudinal direction. Starting with pre-existing ply cracks in off-axis plies, the formation of additional cracks is analyzed by an energy-based approach. A critical laminate energy parameter associated with formation of these cracks is defined and is evaluated using experimental data for a reference cross-ply laminate. The modeling approach requires crack surface displacements, which are calculated by a three-dimensional finite element (3-D FE) analysis performed on a suitable representative volume of the given cracked laminate. The model predictions agree well with experimental data for [0 / ± θ 4 / 0 1 / 2] s and [0 / 90 / ∓ 45] s laminates. A parametric study is conducted to evaluate effects of ply thickness and ply stacking sequence on damage evolution in [0 m / 90 n / ∓ θ p] s laminates.
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Talreja, Ramesh
(författare)
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Department of Aerospace Engineering, Texas A&M University
(creator_code:org_t)
Sammanhörande titlar
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Ingår i:International Journal of Solids and Structures: Elsevier BV47:10, s. 1338-13490020-76831879-2146
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