Energy Absorption in Stitched Composite Sandwich Panels

981202

04/06/1998

Event
Advances In Aviation Safety Conference & Exposition
Authors Abstract
Content
The energy absorption characteristics of a stitched sandwich panel were investigated using experimental and analytical techniques. The structural stability aspects of the proposed mechanism were evaluated using the existing buckling and wrinkling theories. The effect of through-the-thickness stitches on the stability characteristics was investigated using finite element analysis. The configuration of the energy absorption mechanism was based on the stability analysis. The actual energy absorption process was characterized by conducting static crush tests. The experimental results indicated an increase in energy absorption capability with smaller stitch spacing and also resulted in smoother load deflection curves. A broad design guideline was developed for the design of a sandwich panel for energy absorption, based on stability analysis and experimental results.
Meta TagsDetails
DOI
https://doi.org/10.4271/981202
Pages
9
Citation
Raju, K., and Tomblin, J., "Energy Absorption in Stitched Composite Sandwich Panels," SAE Technical Paper 981202, 1998, https://doi.org/10.4271/981202.
Additional Details
Publisher
Published
Apr 6, 1998
Product Code
981202
Content Type
Technical Paper
Language
English