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The Failure of Metals by Fatigue by J Neill Greenwood 1
Fatigue Problems Associated with Aircraft Materials
The Factors Contributing to Fatigue Failure in Aircraft
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aircraft alternating stress amplitude applied axle Battelle Memorial Institute beam bearing alloy bending bolt carbon cause cent components compressive stress corrosion fatigue curve deformation detection determine diameter direction ductile effect elastic endurance limit endurance strength engine experimental extensometer factor of safety fatigue cracks fatigue failure fatigue limit fatigue properties fatigue strength fatigue tests fillet fluctuating fracture frequency hardening inch increase indicated investigation iron laboratory longitudinal machine material maximum stress mean stress measured metal method notch sensitivity number of cycles obtained occur oscillator paper photo-elastic plastic principal stresses problem Proc reduced repeated loading repeated stress residual stresses rotating S-N curve shaft shear stress shot peening shown in Fig specimen static steel strain gauges strength reduction stress concentration factor stress distribution stress raisers structure surface temperature tensile strength tensile stress tension theory thread tion torsion vibration welded wheel seat wire