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One dimensional modelling of failure in laminated plates by delamination buckling

Chai, Herzl and Babcock, Charles D. and Knauss, Wolfgang G. (1981) One dimensional modelling of failure in laminated plates by delamination buckling. International Journal of Solids and Structures, 17 (11). pp. 1069-1083. ISSN 0020-7683. doi:10.1016/0020-7683(81)90014-7.

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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.

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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.
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NASAGrant NSG-1483
Issue or Number:11
Record Number:CaltechAUTHORS:CHAijss81
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Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:21
Deposited By: Wolfgang Gustav Knauss
Deposited On:10 Aug 2004
Last Modified:08 Nov 2021 19:00

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