Ultimate axial load capacity of a delaminated beam-plate
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9231
Reference5 articles.
1. One dimensional modelling of failure in laminated plates by delamination buckling
2. The Energy-Release Rate in the Growth of a One-Dimensional Delamination
3. Effect of delamination of axially loaded homogeneous laminated plates
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