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contributor authorZdeněk P. Bažant
contributor authorIsaac M. Daniel
contributor authorZhengzhi Li
date accessioned2017-05-08T23:50:18Z
date available2017-05-08T23:50:18Z
date copyrightJuly, 1996
date issued1996
identifier issn0094-4289
identifier otherJEMTA8-26979#317_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117030
description abstractMeasurements of the size effect on the nominal strength of notched specimens of fiber composite laminates are reported. Tests were conducted on graphite/epoxy crossply and quasi-isotropic laminates. The specimens were rectangular strips of widths 6.4, 12.7, 25.4 and 50.8 mm (0.25, 0.50, 1.00 and 2.00 in.) geometrically similar in two dimensions. The gage lengths were 25, 51, 102 and 203 mm (1.0, 2.0, 4.0 and 8.0 in.). One set of specimens had double-edge notches and a [0/922 ]s crossply layup, and another set had a single-sided edge notch and a [0/±45/90]s , quasi-isotropic layup. It has been found that there is a significant size effect on the nominal strength. It approximately agrees with the size effect law proposed by Bažant, according to which the curve of the logarithm of the nominal strength versus the logarithm of size represents a smooth transition from a horizontal asymptote, corresponding to the strength criterion (plastic limit analysis), to an inclined asymptote of −0.5 slope, corresponding to linear elastic fracture mechanics. Optimum fits of the test results by the size effect law are obtained, and the size effect law parameters are then used to identify the material fracture characteristics, particularly the fracture energy and the effective length of the fracture process zone. Finally, the R-curves are also identified on the basis of the maximum load data. The results show that in design situations with notches or large initial traction-free cracks the size effect on the nominal strength of fiber composite laminates must be taken into account.
publisherThe American Society of Mechanical Engineers (ASME)
titleSize Effect and Fracture Characteristics of Composite Laminates
typeJournal Paper
journal volume118
journal issue3
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2806812
journal fristpage317
journal lastpage324
identifier eissn1528-8889
keywordsComposite materials
keywordsLaminates
keywordsFracture (Process) AND Size effect
treeJournal of Engineering Materials and Technology:;1996:;volume( 118 ):;issue: 003
contenttypeFulltext


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