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contributor authorLinfa Zhu
contributor authorAditi Chattopadhyay
contributor authorRobert K. Goldberg
date accessioned2017-05-08T21:16:21Z
date available2017-05-08T21:16:21Z
date copyrightJuly 2008
date issued2008
identifier other%28asce%290893-1321%282008%2921%3A3%28132%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45118
description abstractA modified Hashin failure model is developed to characterize different failure modes related to high-velocity impact of composite laminates. Hashin’s compressive fiber failure mode has been extended to consider the shear stress effect. Several micromechanics-based degradation rules are developed and applied to the stress and material property calculations according to different failure modes after the corresponding failure criterion is satisfied. This model has been implemented into a recently developed micromechanics model. Computational results show that this model is able to address shear failure, delamination, and tearing failure observed in the high-velocity impact of composite laminates.
publisherAmerican Society of Civil Engineers
titleFailure Model for Rate-Dependent Polymer Matrix Composite Laminates under High-Velocity Impact
typeJournal Paper
journal volume21
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2008)21:3(132)
treeJournal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 003
contenttypeFulltext


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