A progressive quadratic failure criterion, part B

Kuraishi, Akira; Tsai, Stephen W.; Liu, Kevin K.S.

doi:10.1016/s0266-3538(01)00205-6

Cited by 57 publications

(19 citation statements)

References 5 publications

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“…Puck's action plane concept 13 can be used very well even for nonlinear analysis. Furthermore, the Puck, 13 Tsai, 27 and Zinoviev 29 criteria predict the laminate strength well.…”

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confidence: 88%

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Improved nonlinear stress-strain relation for carbon-epoxy composites and identification of material parameters

Kroupa

Laš

Zemčík

2011

Journal of Composite Materials

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This study focuses on the comparison of selected nonlinear stress-strain relations for unidirectional continuous fiber carbon-epoxy composites and the identification of their parameters under tensile loading. Simple tensile tests of thin strips with various fiber orientations are performed. One linear relation, two types of nonlinear stress-strain relations taken from literature, and one improved relation are analyzed and used within the identification process. All the relationships are deduced from polynomial expansion of complementary energy density. The process, using a combination of the mathematical optimization method and finite element analysis, is described with the necessary details. Failure analysis for the determination of the first failure using Puck's action plane concept is also performed. The tensile and shear strengths are investigated. The comparison of the results obtained from the identified material parameters with the results obtained using the material parameters given by manufacturer is included.

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“…Puck's action plane concept 13 can be used very well even for nonlinear analysis. Furthermore, the Puck, 13 Tsai, 27 and Zinoviev 29 criteria predict the laminate strength well.…”

mentioning

confidence: 88%

“…24 The most successful contributing theories cover the problems of e.g. micromechanical failure (Chamis 25 ), crack density prediction (McCartney, 26 ) or lamina strength prediction (Puck,13 Tsai, 27 Cuntze 28 ). Puck's action plane concept 13 can be used very well even for nonlinear analysis.…”

mentioning

confidence: 99%

Improved nonlinear stress-strain relation for carbon-epoxy composites and identification of material parameters

Kroupa

Laš

Zemčík

2011

Journal of Composite Materials

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“…Liu and Tsai (1998) Kuraishi, Tsai Interactive progressive Tsai and Liu (2002) quadratic failure criterion 14 Wolfe and Butalia (1998) Wolfe Maximum strain energy Butalia and Wolfe (2002) method 15…”

Section: Examples Of Predictions Of Selected Casesmentioning

confidence: 99%

“…Tsai (see Tsai, 1998 andKuraishi et al, 2002) has been associated with the development of failure theories for polymer composites for more than 30 years. He is a strong advocate of the quadratic failure criterion with linear terms (the Tsai-Wu failure criterion) because (i) it is easy to use, (ii) it is a single valued function, (iii) it is based on a mathematically rigorous framework, and (iv) it gives a basis for an extension to cater for three-dimensional failure cases.…”

Section: Examples Of Predictions Of Selected Casesmentioning

confidence: 99%

Progress in failure criteria for polymer matrix composites: A view from the first World-Wide Failure Exercise (WWFE)

Kaddour

Hinton

2010

Failure Mechanisms in Polymer Matrix Composites

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“…[13][14][15][16][17][18][19][20][21][22][23][24][25][26][27] A World Wide Failure Exercise (WWFE) [14][15][16][17][18][19][20][21][22][23][24][25][26][27] conducted by Hinton et al also indicates that there are no failure criteria capable of accurately predicting failure at all levels of analysis, for all loading and boundary conditions, for all failure modes and for all layups, relative thicknesses and constituent materials. 28 The Puck failure criteria 21,29 are considered as the most accurate failure prediction among all the failure criteria observed by WWFE.…”

Section: Introductionmentioning

confidence: 99%

Modified maximum stress failure criterion for composite π joints

Zhao

Qin

Zhang

et al. 2012

Journal of Composite Materials

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Composites are being widely used because of their high strength and stiffness, low density and high formability for creating complex shapes. An all-composite p joint is a structural connector known for its ability to reduce the weight and assembly cost while retaining a good load-carrying capability. Based on the material characteristics of unidirectional fiber composites used in composite p joints, a modified maximum stress failure criterion, which is able to assess damage onset, propagation and final failure, is presented for unidirectional fiber composites. The stiffness and strength of four types of composite p joints under tensile and bending loads are simulated by progressive damage models, involving a finite element analysis, failure criteria and a material degradation model. Numerical results from the application of this criterion in nonlinear element analysis show good agreement with experimental outcomes.

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A progressive quadratic failure criterion, part B

Cited by 57 publications

References 5 publications

Improved nonlinear stress-strain relation for carbon-epoxy composites and identification of material parameters

Improved nonlinear stress-strain relation for carbon-epoxy composites and identification of material parameters

Progress in failure criteria for polymer matrix composites: A view from the first World-Wide Failure Exercise (WWFE)

Modified maximum stress failure criterion for composite π joints

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