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Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads

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Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads. / Ye, J Q ; Sheng, H Y .
In: International Journal of Mechanical Sciences, Vol. 45, No. 8, 08.2003, p. 1309-1326.

Research output: Contribution to Journal/Magazine › Journal article › peer-review

Harvard

Ye, JQ & Sheng, HY 2003, 'Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads', International Journal of Mechanical Sciences, vol. 45, no. 8, pp. 1309-1326. https://doi.org/10.1016/j.ijmecsci.2003.09.017

APA

Ye, J. Q., & Sheng, H. Y. (2003). Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads. International Journal of Mechanical Sciences, 45(8), 1309-1326. https://doi.org/10.1016/j.ijmecsci.2003.09.017

Vancouver

Ye JQ, Sheng HY. Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads. International Journal of Mechanical Sciences. 2003 Aug;45(8):1309-1326. doi: 10.1016/j.ijmecsci.2003.09.017

Author

Ye, J Q ; Sheng, H Y . / Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads. In: International Journal of Mechanical Sciences. 2003 ; Vol. 45, No. 8. pp. 1309-1326.

Bibtex

@article{3c57ca15cde640faa0ecc07fe30a8ad0,
title = "Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads",
abstract = "On the basis of the theory of three-dimensional elasticity, free-edge stresses and displacements of axisymmetrically loaded laminated hollow cylinders are found by using the state space equation method. The study assumes three-dimensional variations of both stresses and displacements and takes into account material constants of all individual material layers. By this approach, composite cylinders may be composed of an arbitrary number of orthotropic layers, each of which may have different material properties and thicknesses. The solution provides a continuous inter-laminar stress field across interfaces and a satisfactory approximation to the singularity occurring in the boundary layer region of a free-edge. Numerical solutions are compared with the results obtained from an alternative numerical method. New results are obtained and parametric studies are carried out. (C) 2003 Elsevier Ltd. All rights reserved.",
author = "Ye, {J Q} and Sheng, {H Y}",
year = "2003",
month = aug,
doi = "10.1016/j.ijmecsci.2003.09.017",
language = "English",
volume = "45",
pages = "1309--1326",
journal = "International Journal of Mechanical Sciences",
issn = "0020-7403",
publisher = "Elsevier Limited",
number = "8",

}

RIS

TY - JOUR

T1 - Free-edge effect in cross-ply laminated hollow cylinders subjected to axisymmetric transverse loads

AU - Ye, J Q

AU - Sheng, H Y

PY - 2003/8

Y1 - 2003/8

N2 - On the basis of the theory of three-dimensional elasticity, free-edge stresses and displacements of axisymmetrically loaded laminated hollow cylinders are found by using the state space equation method. The study assumes three-dimensional variations of both stresses and displacements and takes into account material constants of all individual material layers. By this approach, composite cylinders may be composed of an arbitrary number of orthotropic layers, each of which may have different material properties and thicknesses. The solution provides a continuous inter-laminar stress field across interfaces and a satisfactory approximation to the singularity occurring in the boundary layer region of a free-edge. Numerical solutions are compared with the results obtained from an alternative numerical method. New results are obtained and parametric studies are carried out. (C) 2003 Elsevier Ltd. All rights reserved.

AB - On the basis of the theory of three-dimensional elasticity, free-edge stresses and displacements of axisymmetrically loaded laminated hollow cylinders are found by using the state space equation method. The study assumes three-dimensional variations of both stresses and displacements and takes into account material constants of all individual material layers. By this approach, composite cylinders may be composed of an arbitrary number of orthotropic layers, each of which may have different material properties and thicknesses. The solution provides a continuous inter-laminar stress field across interfaces and a satisfactory approximation to the singularity occurring in the boundary layer region of a free-edge. Numerical solutions are compared with the results obtained from an alternative numerical method. New results are obtained and parametric studies are carried out. (C) 2003 Elsevier Ltd. All rights reserved.

U2 - 10.1016/j.ijmecsci.2003.09.017

DO - 10.1016/j.ijmecsci.2003.09.017

M3 - Journal article

VL - 45

SP - 1309

EP - 1326

JO - International Journal of Mechanical Sciences

JF - International Journal of Mechanical Sciences

SN - 0020-7403

IS - 8

ER -