Buckling and postbuckling of delaminated composites under compressive loads including transverse shear effects
Author:
Affiliation:
1. General Motors Research Laboratories, Warren, Michigan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9894
Reference11 articles.
1. One dimensional modelling of failure in laminated plates by delamination buckling
2. Effect of delamination of axially loaded homogeneous laminated plates
3. Ultimate axial load capacity of a delaminated beam-plate
4. Compressive Stability of Delaminated Random Short-Fiber Composites, Part I—Modeling and Methods of Analysis
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