Pin Reinforcement of Delaminated Sandwich Beams Under Axial Compression
Source abstract
Abstract
The present study is concerned with translaminar reinforcements in a sandwich beam for preventing buckling of the delaminated face sheet under edge-wise axial compression. Sandwich beams consisting of graphite/epoxy face sheets and an aramid honeycomb core were reinforced in the thickness direction using two techniques: Z-pinning using graphite/epoxy pins and a novel “C-pinning technique” developed by the authors. To evaluate the effect of reinforcement type and reinforcement spacing on the ultimate compressive strength of delaminated beams, compression tests were performed. Critical buckling loads and post-buckling behavior of sandwich beams under axial compression were evaluated by finite element analysis to provide insight into the effectiveness of translaminar reinforcement. Pin reinforcement has been shown to significantly improve the ultimate compressive load of a delaminated sandwich beam.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Mechanical Behavior of Composites · Cellular and Composite Structures
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
University of Florida, Department of Aerospace Engineering, Mechanics & Engineering Science, Gainesville, FL 32611, USA
References (8)
Show source-provided references
1. 1. Avery, John L. III, 1998, “Compressive Failure of Delaminated Sandwich Composites,” Master’s Thesis, University of Florida, Gainesville, FL.
2. Avery, J. L. · 1998 · 207
3. 10.1177/00219983000340140210.1177/002199830003401402 ↗
4. Frostig, Y. · 1999 · 23
5. 10.2514/3.1115310.2514/3.11153 ↗
6. Narayanan, M.
7. 7. Narayanan, M., 1999, “Post Buckling of Debonded Sandwich Composite Beams Under Compression,” Master’s Thesis, University of Florida, Gainsville, FL.
8. 8. Sharma, S. K. and Sankar, B. V., 1995, “Effects of Through-the-Thickness Stitching on Impact and Interlaminar Fracture Properties of Textile Graphite/Epoxy Laminates,” NASA Contractor Report CR 195042, Hampton, VA.