Abstract
The observed strength and stress-strain response of [O2/±45] s Thornel-epoxy laminates under varying biaxial-stress ratios are compared with those predicted numerically. Both flat and ring-type off-axis composite specimens are employed by which to generate experimentally the biaxial data. While the numerical predictions tend to overestimate the observed laminate strengths, the several predicted stress-strain curves agree well with each other and with experiment. The off-axis ring specimens produced significantly higher strengths than did the corresponding flat specimens.
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Abbreviations
- σ, τ:
-
stresses
- ε, γ:
-
strains
- E :
-
elastic modulus
- G :
-
shear modulus
- ν:
-
Poisson's ratio
- S ij :
-
compliance
- 1, 2:
-
lamina axes of material symmetry
- x, y :
-
laminate axes of material symmetry
- x′,y′ :
-
rotated coordinate system
- X, Y, S :
-
principal lamina tensile normal and shear strengths
- X*, Y*, S* :
-
principal lamina compressive normal and shear strengths
- u :
-
denotes ultimate value as a subscript or superscript
- θ:
-
off-axis angle
- K 1,K 2,K 6 :
-
coefficients
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Rowlands, R.E. Analytical-experimental correlation of polyaxial states of stress in Thornel-epoxy laminates. Experimental Mechanics 18, 253–260 (1978). https://doi.org/10.1007/BF02324166
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DOI: https://doi.org/10.1007/BF02324166