DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS
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...
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| Format: | Conference or Workshop Item |
| Language: | en |
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2012
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| Online Access: | http://eprints.utem.edu.my/id/eprint/4152/1/SM-13.pdf http://eprints.utem.edu.my/id/eprint/4152/ |
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| _version_ | 1832716033899626496 |
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| author | Said, M. R. Ismail, M. K. Md Akil, H |
| author_facet | Said, M. R. Ismail, M. K. Md Akil, H |
| author_sort | Said, M. R. |
| building | UTEM Library |
| collection | Institutional Repository |
| content_provider | Universiti Teknikal Malaysia Melaka |
| content_source | UTEM Institutional Repository |
| continent | Asia |
| country | Malaysia |
| description | 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%. |
| format | Conference or Workshop Item |
| id | my.utem.eprints-4152 |
| institution | Universiti Teknikal Malaysia Melaka |
| language | en |
| publishDate | 2012 |
| record_format | eprints |
| spelling | my.utem.eprints-41522019-06-03T02:03:37Z http://eprints.utem.edu.my/id/eprint/4152/ DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS Said, M. R. Ismail, M. K. Md Akil, H TJ Mechanical engineering and machinery 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%. 2012-05-29 Conference or Workshop Item PeerReviewed text en http://eprints.utem.edu.my/id/eprint/4152/1/SM-13.pdf Said, M. R. and Ismail, M. K. and Md Akil, H (2012) DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS. In: The 15th International Conference on Applied Mechanics and Mechanical Engineering, 29-31 May 2012, Cairo. |
| spellingShingle | TJ Mechanical engineering and machinery Said, M. R. Ismail, M. K. Md Akil, H DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH PANELS |
| title | DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH
PANELS |
| title_full | DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH
PANELS |
| title_fullStr | DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH
PANELS |
| title_full_unstemmed | DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH
PANELS |
| title_short | DYNAMIC BEHAVIOUR OF PAPER HONEYCOMB SANDWICH
PANELS |
| title_sort | dynamic behaviour of paper honeycomb sandwich
panels |
| topic | TJ Mechanical engineering and machinery |
| url | http://eprints.utem.edu.my/id/eprint/4152/1/SM-13.pdf http://eprints.utem.edu.my/id/eprint/4152/ |
| url_provider | http://eprints.utem.edu.my/ |