1977
DOI: 10.1007/bf02326320
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Ten-deg off-axis test for shear properties in fiber composites

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Cited by 183 publications
(57 citation statements)
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“…However, results in figure 8 showed that the interlaminar strength was lower than in-plane strength at all temperatures, i.e., "-13 (interlaminar) <"-12 (i n-plane) (6) This discrepancy between the prediction and the experiments indicates that the stress concentration could no t be responsible for the difference observed in strength values. Moreover, even if the calculated elastic constants in table III had underestimated the "actual" anisotropy, 8 this conclusion would have still been valid since the anisotropy, which is higher in the interlaminar orientation, is expected to reduce the stress concentration and thus increase the strength of interlaminar specimens.…”
Section: V2 Interlaminar Versus In-plane Shear Strengthmentioning
confidence: 83%
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“…However, results in figure 8 showed that the interlaminar strength was lower than in-plane strength at all temperatures, i.e., "-13 (interlaminar) <"-12 (i n-plane) (6) This discrepancy between the prediction and the experiments indicates that the stress concentration could no t be responsible for the difference observed in strength values. Moreover, even if the calculated elastic constants in table III had underestimated the "actual" anisotropy, 8 this conclusion would have still been valid since the anisotropy, which is higher in the interlaminar orientation, is expected to reduce the stress concentration and thus increase the strength of interlaminar specimens.…”
Section: V2 Interlaminar Versus In-plane Shear Strengthmentioning
confidence: 83%
“…Buckling of specimens was checked by two strain gages which were mounted on the opposite lateral faces. 6 The difference in strain values from these two strain-gages was <3 percent, indicating that the buckling effect on strength values would be small. Force in both specimens was applied along the longitudinal axis by an MTS 7 machine in displacement control with a cross-head speed of 2 /-lm/s.…”
Section: Nasa!tm-2ooo-21 0608mentioning
confidence: 97%
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“…All other results presented in this paper, were obtained using T = 10 5 N/mm 3 . (Chamis and Sinclair 1977;Van Paepegem et al 2006). Experiments show brittle matrix failure.…”
Section: Mixed Mode Bendingmentioning
confidence: 99%