Article ID Journal Published Year Pages File Type
5028826 Procedia Engineering 2017 7 Pages PDF
Abstract

Within this paper, the material behavior of an advanced composite laminate subjected to static cyclic bending loads have been experimentally determined on an LR5KPlus Lloyd Instruments materials testing machine. The composite laminate structure is formed of HELIOPOL 9431ATYX_LSE resin reinforced with five layers STRATIMAT300 glass fibers of 300 g/m2 specific weight. One composite specimen has been subjected to various deflection limits to determine its hysteresis behavior. The results show a maximum hysteresis towards 14 mm upper deflection limit.

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Physical Sciences and Engineering Engineering Engineering (General)
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