DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS
Said, M., Ismail, M., Akil, H. (2012). DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS. EKB Journal Management System, 15(15th International Conference on Applied Mechanics and Mechanical Engineering.), 1-11. doi: 10.21608/amme.2012.37275
M. R. Said; M. K. Ismail; H. Md Akil. "DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS". EKB Journal Management System, 15, 15th International Conference on Applied Mechanics and Mechanical Engineering., 2012, 1-11. doi: 10.21608/amme.2012.37275
Said, M., Ismail, M., Akil, H. (2012). 'DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS', EKB Journal Management System, 15(15th International Conference on Applied Mechanics and Mechanical Engineering.), pp. 1-11. doi: 10.21608/amme.2012.37275
Said, M., Ismail, M., Akil, H. DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS. EKB Journal Management System, 2012; 15(15th International Conference on Applied Mechanics and Mechanical Engineering.): 1-11. doi: 10.21608/amme.2012.37275

DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS

The International Conference on Applied Mechanics and Mechanical Engineering
Article 110, Volume 15, 15th International Conference on Applied Mechanics and Mechanical Engineering., May 2012, Page 1-11  XML PDF (1020.25 K)
Document Type: Original Article
DOI: 10.21608/amme.2012.37275
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Authors
M. R. Said1; M. K. Ismail2; H. Md Akil3
1Professor, Faculty of Mech. Engineering, Universiti Teknikal Malaysia Melaka, Malaysia.
2Postgraduate Student, Faculty of Mech. Eng., Univ. Teknikal Malaysia Melaka, Malaysia.
3Associate Professor, School of Material and Mineral Resources Eng., Engineering Campus, Universiti Sains Malaysia, Malaysia.
Abstract
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 loaddisplacement
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%.
Keywords
Low velocity impact; paper honeycomb sandwich panel; Dynamic loading
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