2017
DOI: 10.3390/ma10050494
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Modelling Behaviour of a Carbon Epoxy Composite Exposed to Fire: Part I—Characterisation of Thermophysical Properties

Abstract: Thermophysical properties of a carbon-reinforced epoxy composite laminate (T700/M21 composite for aircraft structures) were evaluated using different innovative characterisation methods. Thermogravimetric Analysis (TGA), Simultaneous Thermal analysis (STA), Laser Flash analysis (LFA), and Fourier Transform Infrared (FTIR) analysis were used for measuring the thermal decomposition, the specific heat capacity, the anisotropic thermal conductivity of the composite, the heats of decomposition and the specific heat… Show more

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Cited by 40 publications
(32 citation statements)
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References 30 publications
(39 reference statements)
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“…The determination of the kinetic decomposition model was performed in a previous work [ 11 ] and presented in the first-part of this paper [ 24 ]. It is a two-step decomposition model including an autocatalytic reaction being competitive with an nth order reaction [ 24 ]. The material starts to degrade from a virgin state to a (degraded) final state (composed of carbonaceous residue and carbon fibre).…”
Section: Choice Of the 3d Model Usedmentioning
confidence: 99%
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“…The determination of the kinetic decomposition model was performed in a previous work [ 11 ] and presented in the first-part of this paper [ 24 ]. It is a two-step decomposition model including an autocatalytic reaction being competitive with an nth order reaction [ 24 ]. The material starts to degrade from a virgin state to a (degraded) final state (composed of carbonaceous residue and carbon fibre).…”
Section: Choice Of the 3d Model Usedmentioning
confidence: 99%
“…The determination of the physical and thermal properties of materials seems to be the key to obtain a suitable physical model. In the frame, the development of methods to determine thermophysical parameters of the T700/M21 composite was reported in the first-part of the paper [ 24 ].…”
Section: Introductionmentioning
confidence: 99%
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“…Luo et al [33][34][35][36] established a thermomechanical damage model and developed a finite element method using UMATHT and UMAT in ABAQUS, so as to resolve the thermal and mechanic equations for glass/phenolic compound materials withstanding high temperature and thermal radiative surroundings in consideration of the carbonization of sandwich composites, the decomposition of resins, the reduction of elastic modulus, and the delamination of panels and cores. Pauline et al [37][38][39] developed a 3D thermochemical model using SAMCEF software to forecast the temperature contour, the mass loss and the pyrolysis front of a carbon fiber epoxy resin compound laminate (T700/M21 compound material) exposed to high temperature.…”
Section: Introductionmentioning
confidence: 99%
“…Depending on the number of decomposition steps and the scope of the study, single-step or multiple-step kinetic models were used [8][9][10][11]. In the most part, the objectives of using degradation steps were to obtain the best fit between experimental and numerical weight loss curves [12]. e determination of kinetics parameters was centered on developing the least-squares fitting procedure based on DTGA curve measurement at different heating rates [10].…”
Section: Introductionmentioning
confidence: 99%