Large deformation effects in the postbuckling behavior of compositeswith thin delaminations
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/10.2514/3.10153
Reference8 articles.
1. Buckling and postbuckling of delaminated composites under compressive loads including transverse shear effects
2. Ultimate axial load capacity of a delaminated beam-plate
3. One dimensional modelling of failure in laminated plates by delamination buckling
4. 4Yin, W.L., Cylindrical Buckling of Laminated and Delaminated Plates, Proceedings of the 27th SDM AIAA/ASME/ASCE/AHS Conference, AIAA, New York, May 1986, pp.165-179.
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