Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
9717300 | Composites Part B: Engineering | 2005 | 15 Pages |
Abstract
The analysis of the transverse normal stresses demonstrates that the critical failure mode in overlaminated double-lap joints may be related to excessive peel stresses. However, this problem may be alleviated by, e.g. tapering the end of the outer adherends.
Related Topics
Physical Sciences and Engineering
Engineering
Engineering (General)
Authors
Harald Osnes, Dag McGeorge,