Experiments on two notched laminate types show fatigue damage progression differs substantially from quasi-static damage and depends on multi-axiality ratio and notch geometry.
Stiffness degradation of fiber-reinforced composites under uniaxial tensile, pure torsional, and biaxial fatigue at cryogenic temperature
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A Study on the Multi-axial Fatigue Failure Behavior of Notched Composite Laminates
Experiments on two notched laminate types show fatigue damage progression differs substantially from quasi-static damage and depends on multi-axiality ratio and notch geometry.