2007
DOI: 10.1016/j.compstruct.2005.11.031
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Tensile response of graphite/epoxy composites at low temperatures

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Cited by 67 publications
(33 citation statements)
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“…This implied that there is a reduction of ductility and increase in brittleness of the composites at low temperature (Hartwig and Knaak 1984). Kim et al (2007) attributed such increase in brittleness at low temperatures predominantly to the fibers, which increased rapidly within a temperature range from RT to −50 • C. On the other hand, the increase in the laminate strength and stiffness is attributed to the strengthening of the matrix. Therefore, there will be less damage at low temperatures initially, but it continues to increase as the load approaches a critical value where the fibers fail.…”
Section: Tension Test Resultsmentioning
confidence: 96%
“…This implied that there is a reduction of ductility and increase in brittleness of the composites at low temperature (Hartwig and Knaak 1984). Kim et al (2007) attributed such increase in brittleness at low temperatures predominantly to the fibers, which increased rapidly within a temperature range from RT to −50 • C. On the other hand, the increase in the laminate strength and stiffness is attributed to the strengthening of the matrix. Therefore, there will be less damage at low temperatures initially, but it continues to increase as the load approaches a critical value where the fibers fail.…”
Section: Tension Test Resultsmentioning
confidence: 96%
“…A UD laminate model was created in MAC/GMC with material properties from the graphite fiber and epoxy at room temperature, as shown in Table 1. To match the experimental results from Kim et al (2007), the axial fiber modulus was modified until the simulated overall composite axial stiffness agreed with the experimental overall composite axial stiffness at room temperature. This was repeated for all temperatures: 25, − 50, − 100, and − 150 • C, as summarized in Table 2.…”
Section: Validation With Experimental Resultsmentioning
confidence: 99%
“…Kim et al (2007) conducted tensile stiffness experiments with a unidirectional graphite-epoxy-matrix composite from room temperature to − 150 • C. Based on their experimental results docu- Fig. 7 Parametric study of material properties affecting composite global axial CTE of a cross-ply (CP) layup mented in the paper Kim et al (2007), and the result of the parametric studies discussed earlier, the experiment can be simulated in MAC/GMC. A UD laminate model was created in MAC/GMC with material properties from the graphite fiber and epoxy at room temperature, as shown in Table 1.…”
Section: Validation With Experimental Resultsmentioning
confidence: 99%
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