DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS

  • Said M
  • Ismail M
  • Akil H
N/ACitations
Citations of this article
8Readers
Mendeley users who have this article in their library.

Abstract

Low velocity impact tests have been conducted on paper honeycomb sandwich panels. Two panel thicknesses with span length of 100 mm are used; these are 35 mm and 41 mm, respectively. The dynamic behavior of each paper honeycomb thickness is investigated using two types of indentors: hemispherical and bar. The effect of indentor, and specimen length are studied. This includes the pattern of load- displacement curve collapse load and energy absorbed. It concludes that the dynamic collapse load on 41 mm thickness for hemispherical indentor increases by 5% compared with 35 mm. The impact energy absorbed for hemispherical indentor increases by 36%

Cite

CITATION STYLE

APA

Said, M., Ismail, M., & Akil, H. (2012). DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS. The International Conference on Applied Mechanics and Mechanical Engineering, 15(15), 1–11. https://doi.org/10.21608/amme.2012.37275

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free