CORRELATION BETWEEN MICROSTRUCTURE AND FATIGUE PROPERTY OF TI-6AL-4V ALLOY USED IN AEROSPACE APPLICATIONS

EFFECT OF SPECIMEN THICKNESS ON FATIGUE CRACK GROWTH BEHAVIOUR UNDER CONSTANT AND VARIABLE AMPLITUDE LOADING

Low Cycle Fatigue and Crack Initiation Prediction at the Root of a Notch

MECHANICAL AND WEAR BEHAVIOUR OF SOLUTION TREATED Ti-6Al-4V ALLOY

FATIGUE CRACK CLOSURE IN ALUMINIUM ALLOYS UNDER VARIABLE-AMPLITUDE LOADS

EFFECT OF FRONT NOTCH GEOMETRY AND SPECIMEN DIMENSIONS IN DOUBLE TORSION TESTING OF 2124 - T851 ALUMINUM

FATIGUE LIFE PREDICTION OF UN-NOTCHED ROUND SPECIMENS BASED ON CRACKING SIMULATION

BEHAVIOUR OF FATIGUE CRACK PROPAGATION IN Cr - V SPUR GEAR MODEL .

FATIGUE CRACK GROWTH OF STAINLESS STEEL FIBER REINFORCED ALUMINUM COMPOSITES

BEHAVIOUR OF ALUMINIUM- MAGNESIUM ALLOY UNDER ROTATING BENDING FATIGUE TESTS