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A three-dimensional state space finite element solution for laminated composite cylindrical shells

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A three-dimensional state space finite element solution for laminated composite cylindrical shells. / Sheng, H Y ; Ye, J Q .
In: Computer Methods in Applied Mechanics and Engineering, Vol. 192, No. 22-24, 2003, p. 2441-2459.

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

Harvard

Sheng, HY & Ye, JQ 2003, 'A three-dimensional state space finite element solution for laminated composite cylindrical shells', Computer Methods in Applied Mechanics and Engineering, vol. 192, no. 22-24, pp. 2441-2459. https://doi.org/10.1016/S0045-7825(03)00265-2

APA

Sheng, H. Y., & Ye, J. Q. (2003). A three-dimensional state space finite element solution for laminated composite cylindrical shells. Computer Methods in Applied Mechanics and Engineering, 192(22-24), 2441-2459. https://doi.org/10.1016/S0045-7825(03)00265-2

Vancouver

Sheng HY, Ye JQ. A three-dimensional state space finite element solution for laminated composite cylindrical shells. Computer Methods in Applied Mechanics and Engineering. 2003;192(22-24):2441-2459. doi: 10.1016/S0045-7825(03)00265-2

Author

Sheng, H Y ; Ye, J Q . / A three-dimensional state space finite element solution for laminated composite cylindrical shells. In: Computer Methods in Applied Mechanics and Engineering. 2003 ; Vol. 192, No. 22-24. pp. 2441-2459.

Bibtex

@article{cf1a6e60c5bf4224b035ffa5e4b6b20e,
title = "A three-dimensional state space finite element solution for laminated composite cylindrical shells",
abstract = "On the basis of the theory of three-dimensional elasticity, this paper presents a state space finite element solution for stress analysis of cross-ply laminated composite shells. This is a continuation of the authors' previously published work on laminated plates [Compos. Struct. 57 (1-4) (2002) 117; Comput. Methods Appl. Mech. Engrg. 191 (37-38) (2002) 4259]. Once again a state space formulation is introduced to solve for through-thickness stress distributions, while the traditional finite elements are used to approximate the in-surface variations of state variables. A three-dimensional laminated shell element is established in an arbitrary orthogonal curvilinear coordinate system, while the application of the element is shown by calculating stresses in laminated cylindrical shells. Compared with the traditional finite element method, the new solution provides accurate continuous through-thickness distributions of both displacements and and transverse stresses. ",
author = "Sheng, {H Y} and Ye, {J Q}",
year = "2003",
doi = "10.1016/S0045-7825(03)00265-2",
language = "English",
volume = "192",
pages = "2441--2459",
journal = "Computer Methods in Applied Mechanics and Engineering",
issn = "0045-7825",
publisher = "Elsevier",
number = "22-24",

}

RIS

TY - JOUR

T1 - A three-dimensional state space finite element solution for laminated composite cylindrical shells

AU - Sheng, H Y

AU - Ye, J Q

PY - 2003

Y1 - 2003

N2 - On the basis of the theory of three-dimensional elasticity, this paper presents a state space finite element solution for stress analysis of cross-ply laminated composite shells. This is a continuation of the authors' previously published work on laminated plates [Compos. Struct. 57 (1-4) (2002) 117; Comput. Methods Appl. Mech. Engrg. 191 (37-38) (2002) 4259]. Once again a state space formulation is introduced to solve for through-thickness stress distributions, while the traditional finite elements are used to approximate the in-surface variations of state variables. A three-dimensional laminated shell element is established in an arbitrary orthogonal curvilinear coordinate system, while the application of the element is shown by calculating stresses in laminated cylindrical shells. Compared with the traditional finite element method, the new solution provides accurate continuous through-thickness distributions of both displacements and and transverse stresses. 

AB - On the basis of the theory of three-dimensional elasticity, this paper presents a state space finite element solution for stress analysis of cross-ply laminated composite shells. This is a continuation of the authors' previously published work on laminated plates [Compos. Struct. 57 (1-4) (2002) 117; Comput. Methods Appl. Mech. Engrg. 191 (37-38) (2002) 4259]. Once again a state space formulation is introduced to solve for through-thickness stress distributions, while the traditional finite elements are used to approximate the in-surface variations of state variables. A three-dimensional laminated shell element is established in an arbitrary orthogonal curvilinear coordinate system, while the application of the element is shown by calculating stresses in laminated cylindrical shells. Compared with the traditional finite element method, the new solution provides accurate continuous through-thickness distributions of both displacements and and transverse stresses. 

U2 - 10.1016/S0045-7825(03)00265-2

DO - 10.1016/S0045-7825(03)00265-2

M3 - Journal article

VL - 192

SP - 2441

EP - 2459

JO - Computer Methods in Applied Mechanics and Engineering

JF - Computer Methods in Applied Mechanics and Engineering

SN - 0045-7825

IS - 22-24

ER -