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LECTURE No 2 Wednesday September 14th 2 0 p m
LECTURE No 3 Thursday September 15th 2 0 p m
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aircraft alternating aluminium alloys applied austenitic Babbitt bearing alloy bending fatigue butt weld cent compressive stress corrosion fatigue curve diameter direct stress duralumin effect endurance limit endurance ratios factor fatigue behaviour fatigue cracks fatigue failure fatigue limit FATIGUE OF METALS fatigue properties fatigue resistance fatigue strength fatigue stresses fatigue tests ferrous alloys Figure fillet welds fracture frequency fuselage graphite grey cast irons gust heat treated heat treatment high temperatures increase lecture load machine material maximum mean stresses MECHANICAL ENGINEERING mechanical properties mild steel nodular irons notch sensitivity number of cycles obtained occur oycles pearlitic plastic deformation plate pressure reduced repeated stresses residual stresses S-N curve shown shows spar speed square inch strain stress concentration stress range structure surface tensile strength tensile stress test pieces test results testing temperature tons per square Tons/sq tons/sq.in torsional UNIVERSITY OF NOTTINGHAM unnotched vibration welded joints wing wrought