2004
DOI: 10.1299/jsmea.47.8
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Stress Relaxation Behavior of Unidirectional Carbon/Epoxy Composites at Elevated Temperature and Analysis Using Viscoplasticity Model

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Cited by 11 publications
(9 citation statements)
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“…The load relaxation tests carry the advantage of revealing a multitude of strain rates compared to a single strain rate in a steady creep test [ 12 ]. The stress relaxation tests play a major role in revealing the composite materials’ viscoelastic/viscoplastic behaviors [ 40 , 41 , 42 , 43 , 44 , 45 ]. Stress relaxation tests provide the rate of decrease in stress for any state of stress that results from maintaining a constant strain during uniaxial loading.…”
Section: Materials and Experimental Methodsmentioning
confidence: 99%
“…The load relaxation tests carry the advantage of revealing a multitude of strain rates compared to a single strain rate in a steady creep test [ 12 ]. The stress relaxation tests play a major role in revealing the composite materials’ viscoelastic/viscoplastic behaviors [ 40 , 41 , 42 , 43 , 44 , 45 ]. Stress relaxation tests provide the rate of decrease in stress for any state of stress that results from maintaining a constant strain during uniaxial loading.…”
Section: Materials and Experimental Methodsmentioning
confidence: 99%
“…Carbon fiber reinforced epoxy resin composites have excellent mechanical properties and are widely used in aerospace, automotive and other fields 48 . The two sets of experimental data 49 of carbon‐epoxy T800H/3631 with initial stress of 300 and 250 MPa are obtained by static tensile tests at 100°C for fiber orientation 10°.…”
Section: Determination Of Variable‐order Function and Model Predictionmentioning
confidence: 99%
“…The best fitting results of the variable‐order fractional Zener model with four VO functions in describing the stress relaxation behavior of carbon‐epoxy in Reference 49.…”
Section: Determination Of Variable‐order Function and Model Predictionmentioning
confidence: 99%
“…fiber reinforced composite materials; see [6][7][8][9][10][11][12][13]. Kawai et al [8] considered a phenomenological thermoviscoplastic model for investigating the stress-strain field in carbon/epoxy composites at high temperatures. Thermoplasticity theories at finite strains are proposed by Green and Naghdi [14], Casey [15] and Miehe [16].…”
mentioning
confidence: 99%
“…, , ) = 0 is the loading surface in stress space. For a detail comparison of the thermoplasticity constitutive relations for strain space(8) and stress space(17), the loading functions ( , , ) and 8( , , ) are chosen in a Mises's form, respectively i. e.…”
mentioning
confidence: 99%