Tensile strength modeling of glass fiber-polymer composites in fire

被引:86
作者
Feih, S.
Mouritz, A. P.
Mathys, Z.
Gibson, A. G.
机构
[1] Royal Melbourne Inst Technol, Sch Aerosp Mech & Mfg Engn, Melbourne, Vic 3001, Australia
[2] Adv Composite Struct Ltd, Cooperat Res Ctr, Fishermans Bend, Vic 3207, Australia
[3] Def Sci & Technol Org, Platform Sci Lab, Melbourne, Vic 3001, Australia
[4] Univ Newcastle Upon Tyne, Ctr Composite Mat Engn, Newcastle Upon Tyne NE1 7RU, Tyne & Wear, England
关键词
polymer-matrix composites (PMCs); thermomechanical properties; modeling; glass fibers; fire;
D O I
10.1177/0021998307075461
中图分类号
TB33 [复合材料];
学科分类号
摘要
A thermal-mechanical model is presented to calculate the tensile strength and time-to-failure of glass fiber reinforced polymer composites in fire. The model considers the main thermal processes and softening (mechanical) processes of fiberglass composites in fire that ensure an accurate calculation of tensile strength and failure time. The thermal component of the model considers the effects of heat conduction, matrix decomposition and volatile out-gassing on the temperature-time response of composites. The mechanical component of the model considers the tensile softening of the polymer matrix and glass fibers in fire, with softening of the fibers analyzed as a function of temperature and heating time. The model can calculate the tensile strength of a hot, decomposing composite exposed to tire up to the onset of flaming combustion. The thermal-mechanical model is confined to hot, smoldering fiberglass composites prior to ignition. Experimental fire tests are performed on dry fiberglass fabric and fiberglass/vinyl ester composite specimens to validate the model. It is shown that the model gives an approximate estimate of the tensile strength and time-to-failure of the materials when exposed to one-sided heating at a constant heat flux. It is envisaged the model can be used to calculate the tensile softening and time-to-failure of glass-polymer composite structures exposed to fire.
引用
收藏
页码:2387 / 2410
页数:24
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