Journal:Composite Structures
Key Words:Stiffened composite panels； Equivalent stiffness； Buckling； Post-buckling； Failure； Compression test
Abstract:The purpose of this paper was to study the effect of I-shape stiffener stiffness on the buckling and post-buckling, up to collapse behavior of stiffened composite panel under the uniform uniaxial compression load. Six stiffened composite panel configurations, which were orthogonally designed with two skin configurations and three I-shape stiffener configurations, were took into account in the experimental investigation. Three specimens for each configuration (18 specimens in total) were manufactured for test. Before tests, the key dimensions of I-stiffener and skin were measured. Furthermore, all the specimens were also inspected visually and detected by the ultrasonic C-scan system. No initial delamination or debonding area was found on all the specimens according to their C-scan images. The experimental results show that the equivalent compression stiffness of I-shape stiffener has great influence on the buckling load and failure mode of stiffened panel, but a little effect on the fa
Indexed by:Journal paper
Discipline:Engineering
First-Level Discipline:Aeronautical and Astronautical Science and Technology
Document Type:J
Volume:120
Page Number:334-345
Translation or Not:no
Date of Publication:2015-02-01
Co-author:Jiayi Yan,Zhi Chen,Mingbo Tong,Yuequan Wang
Date of Publication:2015-02-01