Published November 1981
| Published
Journal Article
Open
One dimensional modelling of failure in laminated plates by delamination buckling
Abstract
When low speed objects impact composite laminated plates delamination may result. Under inplane compression such delaminations may buckle and tend to enlarge the delaminated area which can lead to loss of global plate stability. This process is modelled here in a first attempt by a delaminating beam-column wherein the local delamination growth, stability and arrest are governed by a fracture mechanics-based energy release rate criterion.
Additional Information
Received 6 November 1980; in revised form 28 January 1981. This work was supported by the National Aeronautics and Space Administration under Grant NSG-1483. The authors are appreciative of this support and wish to acknowledge the encouragement and interest of Dr. James H. Starnes, Jr., NASA Langley, in pursuing this work.Attached Files
Published - CHAijss81.pdf
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CHAijss81.pdf
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Additional details
- Eprint ID
- 21
- Resolver ID
- CaltechAUTHORS:CHAijss81
- Grant NSG-1483
- NASA
- Created
-
2004-08-10Created from EPrint's datestamp field
- Updated
-
2021-11-08Created from EPrint's last_modified field
- Caltech groups
- GALCIT