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contributor authorH. Luo
contributor authorS. Hanagud
date accessioned2017-05-08T21:15:53Z
date available2017-05-08T21:15:53Z
date copyrightOctober 1996
date issued1996
identifier other%28asce%290893-1321%281996%299%3A4%28106%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44835
description abstractIn this paper, modal analysis experiments on composite plates with and without delaminations are carried out. Specimens of the glass cloth and epoxy matrix composite plate, including plates without delamination and plates with through-width delaminations, are manufactured by the layup technique. A thin Teflon film is used to introduce the delamination during the manufacturing process. Delamination modes are found in delaminated plates by comparing the modal analysis results of the delaminated plates with the results of the nondelaminated plates. The sensitivity of the Teflon in the delamination area to the delamination modes is analyzed by the modal analysis experiments of the plates with Teflon in and out of the delamination area. Two delamination coefficients are defined to discern the delamination modes more quantitatively. According to the modal analysis results, the possibility of detecting the delamination size and location is discussed.
publisherAmerican Society of Civil Engineers
titleDelamination Modes in Composite Plates
typeJournal Paper
journal volume9
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1996)9:4(106)
treeJournal of Aerospace Engineering:;1996:;Volume ( 009 ):;issue: 004
contenttypeFulltext


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