Home > Research > Publications & Outputs > Prediction of failure envelopes and stress–stra...

Research

Associated organisational unit

Links

Text available via DOI:

View graph of relations

Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads

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

Published

Standard

Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads. / Ye, Jianqiao; Zhang, Daxu.
In: Journal of Composite Materials, Vol. 46, No. 19-20, 09.2012, p. 2417-2430.

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

Harvard

Ye, J & Zhang, D 2012, 'Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads', Journal of Composite Materials, vol. 46, no. 19-20, pp. 2417-2430. https://doi.org/10.1177/0021998312449678

APA

Ye, J., & Zhang, D. (2012). Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads. Journal of Composite Materials, 46(19-20), 2417-2430. https://doi.org/10.1177/0021998312449678

Vancouver

Ye J, Zhang D. Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads. Journal of Composite Materials. 2012 Sept;46(19-20):2417-2430. doi: 10.1177/0021998312449678

Author

Ye, Jianqiao ; Zhang, Daxu. / Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads. In: Journal of Composite Materials. 2012 ; Vol. 46, No. 19-20. pp. 2417-2430.

Bibtex

@article{89f7aa712d0c4ef9bb7ebc6786ece968,
title = "Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads",
abstract = "This article presents a methodology for predicting the stress–strain response and failure behavior of fiber composite laminates. First, a stress transfer method is proposed by using the concept of the state space equation. The generalized plane strain deformation is assumed in the model. The state space equation was derived by using Fourier series expansions in the width direction and the layer refinement technique through the thickness. Secondly, Christensen{\textquoteright}s stress-based failure criteria are adopted to predict failure of individual plies. Finally, the applications of the methodology are shown by predicting the failure envelopes and stress–strain curves of the test cases provided by the organizers of the Second World-Wide Failure Exercise (WWFE-II). ",
author = "Jianqiao Ye and Daxu Zhang",
year = "2012",
month = sep,
doi = "10.1177/0021998312449678",
language = "English",
volume = "46",
pages = "2417--2430",
journal = "Journal of Composite Materials",
issn = "1530-793X",
publisher = "SAGE Publications Ltd",
number = "19-20",

}

RIS

TY - JOUR

T1 - Prediction of failure envelopes and stress–strain curves of fiber composite laminates under triaxial loads

AU - Ye, Jianqiao

AU - Zhang, Daxu

PY - 2012/9

Y1 - 2012/9

N2 - This article presents a methodology for predicting the stress–strain response and failure behavior of fiber composite laminates. First, a stress transfer method is proposed by using the concept of the state space equation. The generalized plane strain deformation is assumed in the model. The state space equation was derived by using Fourier series expansions in the width direction and the layer refinement technique through the thickness. Secondly, Christensen’s stress-based failure criteria are adopted to predict failure of individual plies. Finally, the applications of the methodology are shown by predicting the failure envelopes and stress–strain curves of the test cases provided by the organizers of the Second World-Wide Failure Exercise (WWFE-II).

AB - This article presents a methodology for predicting the stress–strain response and failure behavior of fiber composite laminates. First, a stress transfer method is proposed by using the concept of the state space equation. The generalized plane strain deformation is assumed in the model. The state space equation was derived by using Fourier series expansions in the width direction and the layer refinement technique through the thickness. Secondly, Christensen’s stress-based failure criteria are adopted to predict failure of individual plies. Finally, the applications of the methodology are shown by predicting the failure envelopes and stress–strain curves of the test cases provided by the organizers of the Second World-Wide Failure Exercise (WWFE-II).

U2 - 10.1177/0021998312449678

DO - 10.1177/0021998312449678

M3 - Journal article

VL - 46

SP - 2417

EP - 2430

JO - Journal of Composite Materials

JF - Journal of Composite Materials

SN - 1530-793X

IS - 19-20

ER -