Skin–Stiffener Separation in T-Stiffened Composite Specimens in Postbuckling Condition
Author:
Affiliation:
1. Research Fellow, Faculty of Aerospace Engineering, Delft Univ. of Technology, 2629 HS, Delft, Netherlands (corresponding author). ORCID: .
2. Professor, Faculty of Aerospace Engineering, Delft Univ. of Technology, 2629 HS, Delft, Netherlands.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000849
Reference23 articles.
1. Buckling Behavior of Composite Laminated Stiffened Panels Under Combined Shear-Axial Compression
2. Progressive failure analyses of compression-loaded composite curved panels with and without cutouts
3. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus
4. Bisagni C. (2006). “Progressive delamination analysis of stiffened composite panels in post-buckling.” Proc. 47th AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. American Institute of Aeronautics and Astronautics Reston VA 1–12.
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