Numerical Investigation to Evaluate Effect of Fiber Orientation on Penetration-Resistance of an Aircraft Composite Material

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 28
  • Download : 0
The effects of the fiber orientation on the penetration-resistance of an aircraft composite material are investigated through experimental and numerical simulation results. Experiments were conducted on cross-ply and quasi-isotropic composite plates with identical boundary conditions. These results are compared with the results of a numerical simulation performed using LS-DYNA. The cross-ply composite plates exhibited the maximum resistance to a low-velocity impact load, with the impactor rebounding, whereas the quasi-isotropic lay-up plates were perforated by the impactor. The FE simulation results show good agreement with the experimental data in the comparisons of the time-force curves, time-energy curves, and impact damage.
Publisher
TAYLOR & FRANCIS INC
Issue Date
2019-10
Language
English
Article Type
Article
Citation

MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, v.26, no.19, pp.1613 - 1621

ISSN
1537-6494
DOI
10.1080/15376494.2018.1444226
URI
http://hdl.handle.net/10203/267480
Appears in Collection
CE-Journal Papers(저널논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0