NASA NTRS · 20060013416
Compressive Failure of Fiber Composites under Multi-Axial Loading
Abstract
This paper examines the compressive strength of a fiber reinforced lamina under multi-axial stress states. An equilibrium analysis is carried out in which a kinked band of rotated fibers, described by two angles, is sandwiched between two regions in which the fibers are nominally straight. Proportional multi-axial stress states are examined. The analysis includes the possibility of bifurcation from the current equilibrium state. The compressive strength of the lamina is contingent upon either attaining a load maximum in the equilibrium response or satisfaction of a bifurcation condition, whichever occurs first. The results show that for uniaxial loading a non-zero kink band angle beta produces the minimum limit load. For multi-axial loading, different proportional loading paths show regimes of bifurcation dominated and limit load dominated behavior. The present results are able to capture the beneficial effect of transverse compression in raising the composite compressive strength as observed in experiments.
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Basu, Shiladitya, Waas, Anthony M., Ambur, Damodar R.. 2006-01-01. Compressive Failure of Fiber Composites under Multi-Axial Loading. https://ntrs.nasa.gov/citations/20060013416
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