1987
DOI: 10.1007/bf00503228
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Thermal expansion of selected graphite-reinforced polyimide-, epoxy-, and glass-matrix composites

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Cited by 13 publications
(12 citation statements)
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“…6 ìå/ o C. 13 These values are typically much smaller than those of matrix materials and so are often considered to be insignificant. 7 The longitudinal CTE of carbon-epoxy composites is regularly cited as being negative 14,15 or zero but again is generally considered negligible in comparison with the transverse CTE. 12,[15][16][17][18] For this reason, and to allow parallels to be drawn with uptake-induced swelling, only transverse thermal expansion will be considered.…”
Section: Thermal Effectsmentioning
confidence: 99%
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“…6 ìå/ o C. 13 These values are typically much smaller than those of matrix materials and so are often considered to be insignificant. 7 The longitudinal CTE of carbon-epoxy composites is regularly cited as being negative 14,15 or zero but again is generally considered negligible in comparison with the transverse CTE. 12,[15][16][17][18] For this reason, and to allow parallels to be drawn with uptake-induced swelling, only transverse thermal expansion will be considered.…”
Section: Thermal Effectsmentioning
confidence: 99%
“…7 The longitudinal CTE of carbon-epoxy composites is regularly cited as being negative 14,15 or zero but again is generally considered negligible in comparison with the transverse CTE. 12,[15][16][17][18] For this reason, and to allow parallels to be drawn with uptake-induced swelling, only transverse thermal expansion will be considered. The transverse CTE may exhibit temperature dependency, 7,8,11,19 particularly when exposure temperatures cross the glass transition temperature.…”
Section: Thermal Effectsmentioning
confidence: 99%
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“…The average fiber modulus reported in the literature for (unsized) P75 21,81,84,86–91 and (sized) P75S 92 is E A = 517 GPa. Using the longitudinal modulus E A = 517 GPa and the properties of Epoxy 934 (Table 3), the rest of elastic properties (ET,GA,νA,νT) for P75 fiber are back calculated by minimizing (equation (6)) between unidirectional lamina data (E1 d,E2 d,G12 d,ν12 d) of both P75/934 and P75/1962 available in literature 19,21,81,83,93 and lamina properties (E1,E2,G12,ν12,ν23) predicted using PMM micromechanics. All the properties of P75 are back calculated using data from literature at RT.…”
Section: Constituent Propertiesmentioning
confidence: 99%