Life estimation model of a cantilevered beam subjected to complex random vibration

ABSTRACT An analytic methodology was developed to predict the fatigue life of a structure ex-periencing stationary, Gaussian random vibration excitation. This method allows theestimation of fatigue life using a frequency domain method, where only the input powerspectral density and damping factor are required. The methodology uses linear elasticfracture mechanics for fatigue crack propagation and accounts for the frequency shiftingthat occurs due to fatigue crack evolution. Good results have been obtained comparingthe analytic model to both finite element analysis (FEA) and experimental results, formild-steel cantilever beams. Keywords damageaccumulation;fatigue;fracture;frequencyshift;powerspectralden-sity; random vibration.NOMENCLATURE A = constant a = crack depth a f = final crack depth C = Paris law constant C ray = statistical correction factor c = half height of rectangular cross-section D ray = equivalent damage constant d = notch depthd a /d N = crack growth rate dt = differential time

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