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A note on a broken layer in an orthotropic laminate composite

Author
Arin, K.
Published
Mar 1, 1974.
Physical Description
1 electronic document
Online Version

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Summary
An orthotropic laminate composite containing a completely broken layer is considered. The problem is formulated in terms of integral transforms and then reduced to a singular integral equation which is solved numerically. The strength of stress singularity at the crack tip is determined from a characteristic equation which is obtained by studying the dominant part of the singular integral equation near the end points. The stress intensity factors are given for various material properties.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19750016783.
Accession ID: 75N24855.
TR-74-4.
NASA-CR-142903.
IFSM-74-59.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15739809