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Edge effects in angle-ply laminated hollow cylinders

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

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Edge effects in angle-ply laminated hollow cylinders. / Ye, J Q .
In: Composite Structures, Vol. 52, No. 2, 05.2001, p. 247-253.

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

Harvard

Ye, JQ 2001, 'Edge effects in angle-ply laminated hollow cylinders', Composite Structures, vol. 52, no. 2, pp. 247-253. https://doi.org/10.1016/S0263-8223(00)00172-0

APA

Ye, J. Q. (2001). Edge effects in angle-ply laminated hollow cylinders. Composite Structures, 52(2), 247-253. https://doi.org/10.1016/S0263-8223(00)00172-0

Vancouver

Ye JQ. Edge effects in angle-ply laminated hollow cylinders. Composite Structures. 2001 May;52(2):247-253. doi: 10.1016/S0263-8223(00)00172-0

Author

Ye, J Q . / Edge effects in angle-ply laminated hollow cylinders. In: Composite Structures. 2001 ; Vol. 52, No. 2. pp. 247-253.

Bibtex

@article{8152855e509a456eb9e69af9c9e269aa,
title = "Edge effects in angle-ply laminated hollow cylinders",
abstract = "The decay rates of stresses and displacements due to self-equilibrated loads acting on the end of angle-ply laminated hollow cylinders are found by using the theory of three-dimensional elasticity. The study assumes that the periodic displacement and stress fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigenmatrix whose eigenvalues represent the decay rates of the problem. By this approach, the composite cylinders may be composed of an arbitrary number of anisotropic layers, each of which may have different material properties, thicknesses and lamination profiles. The decay rates for anti-symmetrically laminated cylinders are found and presented. The effects of material properties, thickness and laminate profiles of cylinders upon the decay rates are investigated for typical anti-symmetric angle-ply laminated cylinders. (C) 2001 Elsevier Science Ltd. All rights reserved.",
author = "Ye, {J Q}",
year = "2001",
month = may,
doi = "10.1016/S0263-8223(00)00172-0",
language = "English",
volume = "52",
pages = "247--253",
journal = "Composite Structures",
issn = "0263-8223",
publisher = "Elsevier Ltd",
number = "2",

}

RIS

TY - JOUR

T1 - Edge effects in angle-ply laminated hollow cylinders

AU - Ye, J Q

PY - 2001/5

Y1 - 2001/5

N2 - The decay rates of stresses and displacements due to self-equilibrated loads acting on the end of angle-ply laminated hollow cylinders are found by using the theory of three-dimensional elasticity. The study assumes that the periodic displacement and stress fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigenmatrix whose eigenvalues represent the decay rates of the problem. By this approach, the composite cylinders may be composed of an arbitrary number of anisotropic layers, each of which may have different material properties, thicknesses and lamination profiles. The decay rates for anti-symmetrically laminated cylinders are found and presented. The effects of material properties, thickness and laminate profiles of cylinders upon the decay rates are investigated for typical anti-symmetric angle-ply laminated cylinders. (C) 2001 Elsevier Science Ltd. All rights reserved.

AB - The decay rates of stresses and displacements due to self-equilibrated loads acting on the end of angle-ply laminated hollow cylinders are found by using the theory of three-dimensional elasticity. The study assumes that the periodic displacement and stress fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigenmatrix whose eigenvalues represent the decay rates of the problem. By this approach, the composite cylinders may be composed of an arbitrary number of anisotropic layers, each of which may have different material properties, thicknesses and lamination profiles. The decay rates for anti-symmetrically laminated cylinders are found and presented. The effects of material properties, thickness and laminate profiles of cylinders upon the decay rates are investigated for typical anti-symmetric angle-ply laminated cylinders. (C) 2001 Elsevier Science Ltd. All rights reserved.

U2 - 10.1016/S0263-8223(00)00172-0

DO - 10.1016/S0263-8223(00)00172-0

M3 - Journal article

VL - 52

SP - 247

EP - 253

JO - Composite Structures

JF - Composite Structures

SN - 0263-8223

IS - 2

ER -