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contributor authorNicolas J. Lombardi
contributor authorJudy Liu
date accessioned2017-05-08T21:16:31Z
date available2017-05-08T21:16:31Z
date copyrightJanuary 2010
date issued2010
identifier other%28asce%290893-1321%282010%2923%3A1%2862%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45201
description abstractGlass fiber-reinforced polymer (GFRP) materials possess inherently high strength-to-weight ratios, but their effective elastic moduli are low relative to civil engineering (CE) construction materials. While elastic modulus may be comparable to that of some CE materials, the lower shear modulus adversely affects stiffness. As a result, serviceability issues are what govern GFRP deck design in the CE bridge industry. An innovative solution to increase the stiffness of a commercial GFRP reinforced-sinusoidal honeycomb sandwich panel was proposed; this solution would completely replace the GFRP honeycomb core with a hexagonal honeycomb core constructed from commercial steel roof decking. The purpose of this study was to perform small-scale tests to characterize the steel hexagonal honeycomb core equivalent elastic moduli in an effort to simplify the modeling of the core. The steel core equivalent moduli experimental results were compared with theoretical hexagonal honeycomb elastic modulus equations from the literature, demonstrating the applicability of the theoretical equations to the steel honeycomb core. Core equivalent elastic modulus equations were then proposed to model and characterize the steel hexagonal honeycomb as applicable to sandwich panel design. The equivalent honeycomb core will enable an efficient sandwich panel stiffness design technique, both for structural analysis methods (i.e., hand calculations) and finite-element analysis procedures.
publisherAmerican Society of Civil Engineers
titleSteel Hexagonal Honeycomb Core Equivalent Elastic Moduli for Bridge Deck Sandwich Panels
typeJournal Paper
journal volume23
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2010)23:1(62)
treeJournal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 001
contenttypeFulltext


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