Show simple item record

contributor authorT. M. Tan
contributor authorC. T. Sun
date accessioned2017-05-08T23:19:31Z
date available2017-05-08T23:19:31Z
date copyrightMarch, 1985
date issued1985
identifier issn0021-8936
identifier otherJAMCAV-26250#6_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99442
description abstractThe low-velocity impact response of graphite/epoxy laminates was investigated theoretically and experimentally. A nine-node isoparametric plate finite element in conjunction with an empirical contact law was used for the theoretical investigation. Theoretical results are in good agreement with strain-gage experimental data. The results of the investigation indicate that the present theoretical procedure describes the impact response of laminate for low-impact velocities.
publisherThe American Society of Mechanical Engineers (ASME)
titleUse of Statical Indentation Laws in the Impact Analysis of Laminated Composite Plates
typeJournal Paper
journal volume52
journal issue1
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3169029
journal fristpage6
journal lastpage12
identifier eissn1528-9036
keywordsComposite materials
keywordsPlates (structures)
keywordsLaminates
keywordsEpoxy adhesives
keywordsFinite element analysis
keywordsGraphite AND Strain gages
treeJournal of Applied Mechanics:;1985:;volume( 052 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record