The axial compressive strength and failure time of unidirectional, viscoelastic composites are investigated. Effects of nonlinear shear behavior and fiber misalignment are emphasized because they are important strength-limiting factors in those strongly anisotropic composites which fail by local buckling in the shear mode of deformation. We first describe the basic buckling model and then, neglecting hereditary effects, predict the compressive strengths of an untoughened and a rubber-toughened carbon/epoxy composite. Next, using a nonlinear viscoelastic constitutive equation for shear behavior, failure time for constant load and compressive strength for increasing load history are predicted by a numerical method. Additionally, approximate analytical formulas are developed which enable one to easily estimate buckling response as a function of initial fiber misalignment angle as well as loading and material parameters.
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November 1993
Review Articles
Compressive Strength and Failure Time Based on Local Buckling in Viscoelastic Composites
R. A. Schapery
R. A. Schapery
Department of Aerospace Engineering and Engineering Mechanics, University of Texas, Austin TX 78712
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R. A. Schapery
Department of Aerospace Engineering and Engineering Mechanics, University of Texas, Austin TX 78712
Appl. Mech. Rev. Nov 1993, 46(11S): S221-S228
Published Online: November 1, 1993
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Online:
April 29, 2009
Citation
Schapery, R. A. (November 1, 1993). "Compressive Strength and Failure Time Based on Local Buckling in Viscoelastic Composites." ASME. Appl. Mech. Rev. November 1993; 46(11S): S221–S228. https://doi.org/10.1115/1.3122640
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