Biaxial and Triaxial Failure Strengths of 6061-T6 Aluminum and AS4/3501-6 Carbon/Epoxy Laminates Obtained by Testing Thickness-Tapered Cruciform Specimens

Armanios, Erian A.; Bucinell, RB; Wilson, DW; Welsh, JS; Adams, DF

doi:10.1520/ctr10919j

J. Compos. Technol. Res.

2001

DOI: 10.1520/ctr10919j

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Biaxial and Triaxial Failure Strengths of 6061-T6 Aluminum and AS4/3501-6 Carbon/Epoxy Laminates Obtained by Testing Thickness-Tapered Cruciform Specimens

Erian A. Armanios¹,

RB Bucinell²,

DW Wilson³

et al.

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Cited by 10 publications

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A survey of test methods for multiaxial and out-of-plane strength of composite laminates

Olsson¹

2011

Composites Science and Technology

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To cite this version:Robin Olsson. A survey of test methods for multiaxial and out-of-plane strength of composite laminates.Composites Science and Technology, Elsevier, 2011, 71 (6) This is a PDF file of an unedited manuscript that has been accepted for publication. As a service to our customers we are providing this early version of the manuscript. The manuscript will undergo copyediting, typesetting, and review of the resulting proof before it is published in its final form. Please note that during the production process errors may be discovered which could affect the content, and all legal disclaimers that apply to the journal pertain. and other textile systems. Tubular and cruciform specimens can provide arbitrary inplane loading, while off-axis and angle-ply specimens provide specific biaxial loadings.Tensile and compressive out-of-plane strength may be determined by axial loading of specimens with a waisted gauge section, while bending of curved specimens allow determination of the out-of-plane tensile strength. Tests suited for out-of-plane shear strength include the short beam shear test, the inclined double notch test and the inclined waisted specimen. Testing of arbitrary tri-axial stress states using tubular or cruciform specimens with superimposed through-the-thickness loading is highly complex and significant problems have been reported in achieving the intended stress states and failure modes. Specific tri-axial stress states can be obtained by uniaxial loading of specimens with constrained expansion, as in the die channel test.

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A survey of test methods for multiaxial and out-of-plane strength of composite laminates

Olsson¹

2011

Composites Science and Technology

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2-D biaxial testing and failure predictions of IM7/977-2 carbon/epoxy quasi-isotropic laminates

Welsh

Mayes

Biskner³

2006

Composite Structures

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Deformation behavior of commercially pure (CP) titanium under equi-biaxial tension

Srinivasan

Velmurugan

Kumar

et al. 2016

Materials Science and Engineering: A

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Biaxial and Triaxial Failure Strengths of 6061-T6 Aluminum and AS4/3501-6 Carbon/Epoxy Laminates Obtained by Testing Thickness-Tapered Cruciform Specimens

Cited by 10 publications

References 6 publications

A survey of test methods for multiaxial and out-of-plane strength of composite laminates

A survey of test methods for multiaxial and out-of-plane strength of composite laminates

2-D biaxial testing and failure predictions of IM7/977-2 carbon/epoxy quasi-isotropic laminates

Deformation behavior of commercially pure (CP) titanium under equi-biaxial tension

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