This paper investigates the effect of mean shear stress on short-beam shear fatigue in a GLARE 1-3/2 commercial fiber–metal laminate (FML). This study explores three shear stress ratios ((Formula presented.) 0.1, 0.3, and 0.5) and two material orientations (longitudinal and transversal) under constant amplitude fatigue. Different stress levels for each (Formula presented.) value were explored to obtain failures between 103 and 106 load cycles. The experimental results reveal anisotropy, with transversal specimens exhibiting lower performance and increased scatter. The mean shear stress effect is discussed herein, with insights into the critical role of mean shear of fatigue performance. (Formula presented.) 0.1 was the most severe condition and (Formula presented.) 0.5 was the least severe. The (Formula presented.) 0.3 condition produced steeper S-N curves, indicating that the combined effect of mean shear stress and shear stress amplitude led to a higher rate of damage accumulation. The fractographic analysis investigated the failure modes and confirmed the damage dominated by Mode II, supporting the test methodology employed.

Short-Beam Shear Fatigue Behavior on Unidirectional GLARE: Mean Shear Stress Effect, Scatter, and Anisotropy

Castrodeza, Enrique M.
2025-01-01

Abstract

This paper investigates the effect of mean shear stress on short-beam shear fatigue in a GLARE 1-3/2 commercial fiber–metal laminate (FML). This study explores three shear stress ratios ((Formula presented.) 0.1, 0.3, and 0.5) and two material orientations (longitudinal and transversal) under constant amplitude fatigue. Different stress levels for each (Formula presented.) value were explored to obtain failures between 103 and 106 load cycles. The experimental results reveal anisotropy, with transversal specimens exhibiting lower performance and increased scatter. The mean shear stress effect is discussed herein, with insights into the critical role of mean shear of fatigue performance. (Formula presented.) 0.1 was the most severe condition and (Formula presented.) 0.5 was the least severe. The (Formula presented.) 0.3 condition produced steeper S-N curves, indicating that the combined effect of mean shear stress and shear stress amplitude led to a higher rate of damage accumulation. The fractographic analysis investigated the failure modes and confirmed the damage dominated by Mode II, supporting the test methodology employed.
2025
fiber–metal laminate; GLARE; interlaminar shear; mean shear stress effect; short-beam shear fatigue;
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1304081
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