Fatigue Behaviour of Fibre Metal Laminate (Glare) Vis-À-Vis Plain Aerospace Aluminum Alloy: An Experimental Investigation

Sunil Bhat

doi:10.4028/www.scientific.net/AMM.310.7

Paper Titles

Experimental Studies on Dispersion of Fine Non-Spherical Particles in Enclosed Spaces
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Fatigue Behaviour of Fibre Metal Laminate (Glare) Vis-À-Vis Plain Aerospace Aluminum Alloy: An Experimental Investigation
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The Effects of Chitosan on Dyeing Abilities of Cotton Fabric Dyed with Reactive Dyes
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Proposal of Implementation of Conductive Polymer Composites as High Temperature Detection Devices for LVSB’s
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Study on the Preparation of a New Tofu Coagulant by the Acidic Components of Schisandra
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Synthesis and Properties of IPDI-TMP Waterborne Curing Agent
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Experimental Study on Gas Production from Methane Hydrate Bearing Sand by Depressurization
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Response of Alfalfa (Medicago sativa L.) Bud Seedling to Saline and Alkaline Stress under Water Culture Conditions
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 310Fatigue Behaviour of Fibre Metal Laminate (Glare)...

Fatigue Behaviour of Fibre Metal Laminate (Glare) Vis-À-Vis Plain Aerospace Aluminum Alloy: An Experimental Investigation

Abstract:

Performance of cracked fibre metal laminate (Glare) under fatigue load differs from that of cracked plain aerospace aluminum alloy. Load transfer towards stronger fibres in Glare shields crack tips in aluminum layers that retards fatigue crack growth rates. The paper experimentally investigates the fatigue behaviour of Glare at variable stress ratio’s in an ambient environment for comparison with that of plain aerospace aluminum alloy.