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A laminate composite with a crack normal to the interfaces

โœ Scribed by P.D. Hilton; G.C. Sih

Publisher
Elsevier Science
Year
1971
Tongue
English
Weight
914 KB
Volume
7
Category
Article
ISSN
0020-7683

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๐Ÿ“œ SIMILAR VOLUMES

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Zero thickness crack tip interface elements for a crack normal to the interface between two materials are presented. The elements are shown to have the desired r\*-' (0 < I < 1) singularity in the stress field at the crack tip and are compatible with other singular elements. The stiffness matrices o

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An anisotropic composite laminate containing a part-through crack parallel to the fiber direction is analyzed. The composite laminate is modeled as an assembly of cracked and untracked plates bonded by a thin resin-rich layer. The cracked plate is considered to contain a through crack of finite leng