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ASSESSMENT OF DYNAMIC FRACTURE PROPAGATION RESISTANCE
FACTORS AFFECTING THE DESIGN OF MILITARY AIRCRAFT
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alloy analysis applied assessment ASTM bend calculated compact tension component constant correlation crack extension crack growth crack growth rate crack initiation crack length crack propagation crack tip creep criterion curve cyclic damage tolerance defects deformation determined disc displacement ductile dynamic fracture effect elastic energy equation evaluation experimental failure fatigue crack growth Fatigue CTOD test FCP test finite element finite element analysis flaw fracture mechanics fracture toughness frequency fringe function grain impact increase Inspection KEYWORDS linear linear elastic load martensitic material maximum measured method notch number of cycles obtained parameters photoelastic plane plane strain plastic zone plate plotted pre-cracking predicted pressure vessel procedure range ratio residual strength ringdown shear band shear stress shown in Fig shows steel strain rate stress amplitude stress field stress intensity factor structure Table technique temperature tensile thickness turbine values velocity welded joints wind turbine yield yield strength