Edge effects in cross-ply laminated hollow cylindrical shells

School of Engineering

Associated organisational unit

Manufacturing

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review

Published

Standard

Edge effects in cross-ply laminated hollow cylindrical shells. / Ye, J Q .
Computational techniques for materials, composites and composite structures. ed. / BHV Topping. Edinburgh: Civil-Comp Press, 2000. p. 359-363.

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review

Harvard

Ye, JQ 2000, Edge effects in cross-ply laminated hollow cylindrical shells. in BHV Topping (ed.), Computational techniques for materials, composites and composite structures. Civil-Comp Press, Edinburgh, pp. 359-363, 5th International Conference on Computational Structures Technology/2nd International Conference on Engineering Computational Technology, LEUVEN, 6/09/00.

APA

Ye, J. Q. (2000). Edge effects in cross-ply laminated hollow cylindrical shells. In BHV. Topping (Ed.), Computational techniques for materials, composites and composite structures (pp. 359-363). Civil-Comp Press.

Vancouver

Ye JQ. Edge effects in cross-ply laminated hollow cylindrical shells. In Topping BHV, editor, Computational techniques for materials, composites and composite structures. Edinburgh: Civil-Comp Press. 2000. p. 359-363

Author

Ye, J Q . / Edge effects in cross-ply laminated hollow cylindrical shells. Computational techniques for materials, composites and composite structures. editor / BHV Topping. Edinburgh : Civil-Comp Press, 2000. pp. 359-363

Bibtex

@inproceedings{4a2a5fced64344199e52912e99463511,

title = "Edge effects in cross-ply laminated hollow cylindrical shells",

abstract = "The edge effects of self-equilibrated loads acting on the end of cross-ply laminated hollow cylinders are investigated by using three dimensional elasticity theory. The study assumes that the periodic displacement and stresses fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigen-matrix whose eigenvalues represent the decay rates of the problem. The decay rates for either symmetric or antisymmetric cross-ply laminated cylinders are found and presented. The effects of material properties on decay rates are investigated for a typical eight-layered antisymmetric cross-ply laminated cylinder.",

author = "Ye, {J Q}",

year = "2000",

language = "English",

isbn = "0948749695",

pages = "359--363",

editor = "BHV Topping",

booktitle = "Computational techniques for materials, composites and composite structures",

publisher = "Civil-Comp Press",

address = "United Kingdom",

note = "5th International Conference on Computational Structures Technology/2nd International Conference on Engineering Computational Technology ; Conference date: 06-09-2000 Through 08-09-2000",

}

RIS

TY - GEN

T1 - Edge effects in cross-ply laminated hollow cylindrical shells

AU - Ye, J Q

PY - 2000

Y1 - 2000

N2 - The edge effects of self-equilibrated loads acting on the end of cross-ply laminated hollow cylinders are investigated by using three dimensional elasticity theory. The study assumes that the periodic displacement and stresses fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigen-matrix whose eigenvalues represent the decay rates of the problem. The decay rates for either symmetric or antisymmetric cross-ply laminated cylinders are found and presented. The effects of material properties on decay rates are investigated for a typical eight-layered antisymmetric cross-ply laminated cylinder.

AB - The edge effects of self-equilibrated loads acting on the end of cross-ply laminated hollow cylinders are investigated by using three dimensional elasticity theory. The study assumes that the periodic displacement and stresses fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigen-matrix whose eigenvalues represent the decay rates of the problem. The decay rates for either symmetric or antisymmetric cross-ply laminated cylinders are found and presented. The effects of material properties on decay rates are investigated for a typical eight-layered antisymmetric cross-ply laminated cylinder.

M3 - Conference contribution/Paper

SN - 0948749695

SP - 359

EP - 363

BT - Computational techniques for materials, composites and composite structures

A2 - Topping, BHV

PB - Civil-Comp Press

CY - Edinburgh

T2 - 5th International Conference on Computational Structures Technology/2nd International Conference on Engineering Computational Technology

Y2 - 6 September 2000 through 8 September 2000

ER -

Research

Associated organisational unit